N641GT

Part: SLIDE — ACTIVATED (ZONE 800) · airframe 98,258 hrs · 27,331 cycles

R4 ENTRY DOOR SLIDE ACTIVATED DUE TO FLT ATTENDANT INADVERTENT OPENING, DOOR ARMED. R & R DOOR SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 98,145 hrs · 27,305 cycles

L4 JUMPSEAT FLASHLIGHT OR BATTERY NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT BATTERY REF AMM 25-64-00. OPS CHECK GOOD.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 97,896 hrs · 27,250 cycles

R1 DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED ESCAPE SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED.

Part: LIGHT — DISCONNECTED (ZONE 200) · airframe 97,157 hrs · 27,096 cycles

R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE.(<P>FOUND R1 EMERGENCY EXIT SIGN LIGHT PLATE DISCONNECTED IAW WDM 33-51-14. RESECURED CONNECTOR AND LIGHT OPS CHECK GOOD IAW B767 AMM 33-51-09.</P>)

Part: PBE — MISSING (ZONE 200) · airframe 96,533 hrs · 26,955 cycles

PBE AT R4 DOOR MISSING TAMPER SEAL.(<P>R/R PBE IAW AMM 25-64-00-01. NO FURTHER DEFECTS NOTED. DMI 224468 CLOSED. REF IPC 25-64-54-19. OSD: 1/23/2025

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 96,531 hrs · 26,954 cycles

R1 RIGHT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. INSTALLED SHIM ON GIRT BAR FITTING AND BEARING ASSY IAW AMM 52-11-00/501 AND IPC 52-11-41-01. OPS CHECK GOOD. DOOR ARMS PROPERLY.</P>)

Part: ACTUATOR — FAULTED (SPOILERS) · airframe 96,527 hrs · 26,952 cycles

LH OVERWING EXIT INOP (MAIN ENTRY DOORS/SLIDES/EMERGENCY).(<P>R/R LEFT WING SPOILER BLOW DOWN ACTUATOR PER AMM 25-65-20. OPS CHECK GOOD. DMI 224324 CLOSED</P>)

Part: ANTENNA — CORRODED (ZONE 200) · corrosion level 2 · airframe 96,527 hrs · 26,952 cycles

CORROSION ON BASE ANTENNA TCAS UPPER FUSELAGE(<P>TCAS ANTENNA WAS REPLACED WITH SATISFACTORY TEST IAW AMM 34-45-02-344-158. TORQUE APPLIED 20-LB-IN S/N 924401137 DATE 30/SEP/25 BONDING METTER 0.8 MILLI OHM S/N 80005870</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 96,527 hrs · 26,952 cycles

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(<P>FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW SRM 53-10-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: INLET — CORRODED (ZONE 400) · corrosion level 2 · airframe 96,527 hrs · 26,952 cycles

ENG 1, INLET COWL, ZONE 411, WITH POINTS OF CORROSION INNER ACCESS 412, AT INNER BARREL SKIN SURFACE, AT 12 HRS POSITION.(<P>&NBSP;ENG 1, INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED</P>)

Part: INLET — CORRODED (ZONE 400) · corrosion level 2 · airframe 96,527 hrs · 26,952 cycles

CORROSION AT ENG 1 INLET COWL, INBD SIDE (INSIDE ACCESS PANEL) AT 8:00 O'CLOCK.(<P>ENG 1 INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED.</P>)

Part: PCA — LEAKING (ZONE 300) · airframe 96,527 hrs · 26,952 cycles

RUDDER, LOWER PCA WITH HYDRAULIC LEAK.(<P>RUDDER, LOWER PCA WAS ADJUSTED PER AMM 27-21-02-422-038. LEAK CHK GOOD. NO FURTHER DEFECTS NOTED.</P>)

Part: FIRE SEAL — DAMAGED (ZONE 400) · airframe 96,527 hrs · 26,952 cycles

ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD WITH SEALANT DAMAGE.(<P>ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD SEALANT WAS RESTORED IAW AMM 78-31-00-308-072-H00. NO FURTHER DEFECTS NOTED</P>)

Part: WEDGE — BUCKLED (ZONE 500 SLAT) · airframe 96,527 hrs · 26,952 cycles

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 28'' FROM INBD EDGE AND 11'' FROM TE.(<P>LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE AT 28'' FROM INBD EDGE AND 11'' FROM TE WAS REPAIRED IAW SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 96,527 hrs · 26,952 cycles

LEFT WING, INBOARD FLAP LOWER AREA BTW WS 314 AND WS404 WITH DELAMINATION.(<P>LEFT WING INBOARD FLAP LOWER AREA WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)

Part: FIRE SEAL — WORN (ZONE 400) · airframe 96,527 hrs · 26,952 cycles

ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WITH WEAR.(<P>ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

Part: BULB — NO TEST (ZONE 200) · airframe 96,527 hrs · 26,952 cycles

EMERGENCY LIGHTS TEST, EMERGENCY LIGHT OF CEILING PANELS ROWS 16 LH AND 19 RH INOP(<P>EMERGENCY LIGHTS OF CEILING PANELS ROWS 16 LH AND 19 RH BULBS WERE REPLACED IAW AMM 33-51-04-002-001. OPS CHK GOOD</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 96,527 hrs · 26,952 cycles

SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(<P>SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW SRM 53-10-01-2R-1. NO FURTHER DEFECTS NOTED.

Part: BOLT — LOOSE (SLIDE) · airframe 96,527 hrs · 26,952 cycles

REMOVAL AND INSTALATION OF SLIDE ON LEFT WING FOR ACCESS LOOSE BOLT(<P>THE LOOSE BOLT OF SLIDE ON LEFT WING WAS INSTALLED CORRECTLY IAW AMM 20-11-00-910-802. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — MECHANIC ERROR (ZONE 200) · airframe 96,527 hrs · 26,952 cycles

MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD BETWEEN BSTA 933 TO BSTA 938.5 AND WL185.2 AT BBL 97.42.(<P>MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD BETWEEN BSTA 933 TO BSTA 938.5 AND WL185.2 AT BBL 97.42. WAS REPAIRED IAW TRE 6753710 &AMP; FAA FORM 8100-9. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 96,527 hrs · 26,952 cycles

LH WING, UPPER SURFACE, BETWEEN REAR SPAR AND STGR L-10, WBL 97.9566 WITH CORROSION(<P>THE CORROSION AREA WAS REPAIRED BY INSTALLING 2 REPAIR DOUBLERS, 1 SKIN FILLER AND STRINGER SEGMENTS. THIS REPAIR INSTRUCTION WERE PROVIDED ON BOEING MESSAGE CMA-TLS-24 0218 &AMP; TRE 6757272. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — LEAKING (ZONE 500) · airframe 96,527 hrs · 26,952 cycles

FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITTING.(<P>FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITTING WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED.</P>)

Part: FUEL TANK — LEAKING (ZONE 600) · airframe 96,527 hrs · 26,952 cycles

RIGHT WING, DRY BAY WITH FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9(<P>FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9 RIGHT WING, RIGHT WING, DRY BAY WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED</P>)

Part: LINER — BROKEN (ZONE 800) · airframe 96,527 hrs · 26,952 cycles

BROKEN LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR.(<P>LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR. WAS REPAIRED IAW AMM 25-00-00-308-166. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CORRODED (ZONE 300) · airframe 96,527 hrs · 26,952 cycles

LEFT HORIZONTAL STABILIZER TIP UPPER SURFACE WITH LIGHT CORROSION AT 4.5'' FROM TRAILING EDGE.(<P>STABILIZER TIP UPPER SURFACE AT 4.5'' FROM TRAILING EDGE BASE DISCHARGER WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: PUMP — CORRODED (ZONE 600) · airframe 96,527 hrs · 26,952 cycles

RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION(<P>RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION WAS REPLACED PER AMM 28-22-03-004-001. OPS CHK GOOD</P>)

Part: CONNECTOR — CORRODED (ZONE 200) · airframe 96,527 hrs · 26,952 cycles

UPPER HALF OF FUSELAGE, TOP TCAS ANTENNA, FOUR CONNECTORS, WITH CORROSION.(<P>CONNECTORS WERE CLEANED AS CLIENT REQUIREMENT, CORROSION INHIBITING COMPOUND AV25 WAS USED AS PROTECION AGENT IAW SWPM 20-60-03. NO FURTHER DEFECTS NOTED</P>)

Part: WEDGE — BUCKLED (ZONE 500 SLAT) · airframe 96,527 hrs · 26,952 cycles

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 45'' FROM INBD EDGE AND 11'' FROM TE.(<P>LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE AT 45'' FROM INBD EDGE AND 11'' FROM TE WAS REPAIRED SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED</P>)

Part: ESCAPE HATCH — OUT OF ALIGNMENT (ZONE 800) · airframe 96,393 hrs · 26,922 cycles

RIGHT OVERWING ESCAPE STEP MISALIGNED(<P><SPAN>REMOVED RIGHT AFT EMERGENCY ESCAPE HATCH. REALIGNED ESCAPE STEP, REINSTALLED RIGHT AFT EMERGENCY HATCH PER AMM 52-21-01</SPAN></P>)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 98,562 hrs · 26,855 cycles

1 EA OVERHEAD EMER LT INOP NEAR 30AC(<P>RELAMPED 1 EA EMER LT 30AC &AMP; OPS CHK OK IAW AMM 33-51-07</P>)

Part: BRACKET — DAMAGED (ZONE 200) · airframe 95,788 hrs · 26,790 cycles

AFT MEGAPHONE BRACKET DAMAGE LH AFT CLOSET(<P>REMOVED DAMAGED BRACKET ASSY AT AFT MEGAPHONE BY LH AFT CLOSET, MD. LOCATED, CLEARED, PREPARED, SECURED AND INSTALLED NEW BRACKET ASSY, PER BOEING 767 SRM 51-40-02-06-0</P>)

Part: OXYGEN BOTTLE — DAMAGED (ZONE 200) · airframe 95,788 hrs · 26,790 cycles

FWD CLOSET PORTABLE OXYGEN BOTTLE MFG LABEL DAMAGE P/N 9700C1A-BF23A(<P>REMOVED AND REPLACED PORTABLE OXYGEN CYLINDER LOCATED IN CABIN FWD CLOSET AS REQUIRED IAW AMM&NBSP;</P> / <P>35-11-01. OPS &AMP; LEAK CHECK GOOD</P>)

Part: BOLT — LOOSE (ZONE 400) · airframe 95,788 hrs · 26,790 cycles

ENGINE # 1 AFT NACELLE O/B ACCESS DOOR REAR HINGE FITTING WITH BOLT LOOSE(<P>REMOVED DAMAGE ANGLE AT ENG 1, AFT NACCELLE O/B ACCESS DOOR REAR HINGE FITTING AREA, LOCATED, CLEANED, PREPARED, DRILLED, SECURED AND INSTALLED NEW ANGLE, COMPLETED ASSEMBLY, NO FURTHER DISCREPANCIES NOTED, AT ENG #1, AFT NACCELE O/B ACCESS DOOR REAR HINGE, PER BOEING 767 SRM&NBSP;</P> / <P>51-40-02-0G-0</P>)

Part: CAP — UNKNOWN · airframe 95,788 hrs · 26,790 cycles

ENGINE #2 INB T/R VALVE TO OPEN AND CLOSE C/DUCT INOP.(<P>REMOVED AND REPLACED OPENING VALVE AT #2 REVERSER INBOARD HALF IAW AMM 78-31-03. INSTALLED REVERSER COWLING OPENING FITTING DUST CAP &AMP; OPS CHECK OK&NBSP;</P>)

Part: LATCH — LOOSE (NACELLE DOOR) · airframe 95,788 hrs · 26,790 cycles

ENG #2 NACELLE STRUT INBOARD DOOR WITH LATCH LOOSE(<P>LOCATED, CLEANED, PREPARED &AMP; REMOVED ADJUSTABLE BOLT &AMP; SAFETY WIRE, PROCEED TO PERFORM ADJUSTMENT, RIGGING AS REQUIRE, RESECURED AND RE-INSTALL BOLT AFTER VERIFIED. NO FURTHER DISCREPANCIES. PERFORM SAFETY WIRE AS PER B767-300 SRM 51-40-02-0G-0 &AMP; AMM 20-10-23-964-001.</P>)

Part: FIRE BOTTLE — LEAKING (NOT REPORTED) · airframe 95,749 hrs · 26,783 cycles

FIRE BOTTLE LEAKED(<P>REMOVED AND REPLACED FIRE BOTTLE IAW EO 6725A252. OK FOR SERVICE</P>)

Part: SIGN — DISCONNECTED (ZONE 200) · airframe 97,157 hrs · 27,096 cycles

R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. FOUND R1 EMERGENCY EXIT SIGN PLATE DISCONNECTED. RECONNECTED PER WDM 33-51-14. OPS CHECK GOOD PER AMM 33-51-09.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,204 hrs · 26,658 cycles

DURING OPERATIONAL TEST EXTERIOR EMERGENCY LIGHTS, THREE RIGHT REAR LIGHTS DO NOT OPERATE IN STA 1197, STA 1219, AND 1562.(<P>THE M733 POWER SUPPLY BATTERY PACK WAS CHANGED PER AMM 24-54-00. OPS CHK GOOD.</P>)

Part: SWITCH — FAULTED (EMERGENCY LIGHTS) · airframe 95,204 hrs · 26,658 cycles

DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS FOUND WITH FAIL(<P>EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS REPLACED PER AMM 33-51-00. NO FURTHER DEFECTS NOTED.</P>)

Part: SIGN — LOOSE (OVERWING) · airframe 95,131 hrs · 26,641 cycles

LEFT OVERWING EMERGENCY EXIT SIGN FOUND LOOSE(<P>RE-SECURED LEFT WING EMERGENCY EXIT SIGN. SECURED IAW AMM 33-51-01</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,332 hrs · 26,456 cycles

LI-ION EXTINGUSHING AGENT P/N LKFD IN RH SIDE LAST OVERHEAD BIN FOUND LEAKING NEEDS REPLACMENT(<P>REMOVED AND REPLACED LI-ION EXTINGUISHING AGENT REFERENCE ATLAS AIR EMERGENCY EQUIPMENT CONFIGURATION - 641GT&NBSP;</P>)

Part: PBE — UNKNOWN (UNKNOWN) · airframe 94,040 hrs · 26,397 cycles

L1 PBE INDICATOR STRIP SHOWS RED(<P><SPAN>REMOVED AND REPLACED PBE AT L1 DOOR IAW AMM 25-64-00</SPAN></P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,938 hrs · 26,374 cycles

CAPT & F/O EVAS INOP(<P>INSTALLED NEW EVAS SECURITY SEAL STICKERS IAW EO6725A222. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,882 hrs · 26,363 cycles

FLIGHT ATTENDANT SEAT L4A PSU INOP.(<P>TRANSFER TO MDDR 189255 PER MEL 35-21-01-01A CAT B, DUE DATE 7/17/2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER FUSELAGE SKIN BETWEEN STA 266.5 / STA 276 AND S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER FUSELAGE SKIN BETWEEN STA 456 / STA 478 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER HALF FUSELAGE SKIN BETWEEN STA 412 / STA 434 AND STRINGER S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

FUEL LEAK ON PORT OF DRY BAY AT LH WING TANK(<P>FUEL LEAK WAS REPAIRED ON PORT OF DRY BAY AT LH WING TANK THE FUEL LEAK TEST WAS SATISFACTORY PER AMM 28-11-00-30-8-013</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

LH FUSELAGE SKIN BETWEEN STA 158.2 AND BELOW WL220 WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS</P>)

Part: CARRIER ASSY — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

RH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER FUSELAGE SKIN BETWEEN STA 566 / STA 588 AND S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

FUSELAGE SKIN BETWEEN STA 157 AND STRINGER S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

FUSELAGE SKIN BETWEEN STA 132 / STA 143 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER HALF FUSELAGE SKIN AT STA 266.5 AND STRINGER S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

FUSELAGE SKIN BETWEEN STA 143 / STA 157 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,854 hrs · 26,356 cycles

CORROSION ON KEEL BEAM HORIZONTAL WEB BETWEEN STA 785.9 / STA 880(<P>REPAIR WAS ATTENDED BY SR 3-5696704793 (MXA EO TRE6753615) APPROVED BY FAA FORM 8100-9</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER HALF FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND STRINGER S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P>&NBSP;LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

UPPER HALF FUSELAGE SKIN AT STA 287 AND STRINGER S-1 LH / S-2 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: CARRIER ASSY — UNKNOWN (UNKNOWN) · airframe 93,854 hrs · 26,356 cycles

RH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

Part: LENS — DAMAGED · airframe 93,796 hrs · 26,343 cycles

L1 DOOR LOWER EXIT LIGHT HA BURNT OUT BULBS(<P>DURING REPLACEMENT FOUND EXIT SIGN HAS DAMAGED CLIP REMOVED AND REPLACED LENS COVER IAW 33-51-8. OK FOR SERVICE.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,693 hrs · 26,315 cycles

L1 EXIT SIGN LOOSE.(<P>SECURED L1 EXIT SIGN IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE · airframe 93,336 hrs · 26,244 cycles

EXIT LIGHT ASSY AT L4 BROKEN.(<P>REMOVED AND REPLACED EXIT LIGHT ASSY AT L4 PER B767 AMM 33-51-01</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

AFT CARGO DOOR, REAR UPPER STOP LOOSE .(<P>RETORQUED AFT CARGO DOOR REAR UPPER STOP PER AMM 20-11-00.</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 OUT OF SERVICE DATE(<P>REMOVED AND REPLACED L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 AS REQUIRED IAW B767 AMM 35-21-04.</P>)

Part: PIN — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

LEFT OFF WING SLIDE INFLATION BOTTLE, P/N WARNING STREAMER DAMAGED .(<P>REPLACED PIN WITH STREAMER IAW 767 AMM 25-65-00-442-410 STEP 10</P>)

Part: ANTENNA — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

LOWER FUSELAGE, DME ANTENNA WITH PAINT DAMAGED AT L/E.(<P>REPLACED DME #1 SYS ANTENNA &AMP; OPS CHECK DME SYS OK PER AMM 34-55-02.</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 OUT OF SERVICE DATE(<P>REMOVED&NBSP; AND REPLACED&NBSP; L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 AS REQUIRED IAW B767 AMM 35-21-04.</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

PASSENGER CABIN NUMEROUS BIO-HAZARD KITS OUT OF SERVICE DATE P/N 500094 .(<P>REMOVED &AMP; REPLACED NUMEROUS BIO HAZARD KITS AS REQUIRED IN PAX CABIN PER 767 AMM 25-64-00. OPS CHECK OK.</P>)

Part: LATCH — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

ENG #2 NACELLE STRUT EXTERNAL ACCESS DOOR REAR LATCH BROKEN(<P>REMOVED DAMAGED 4EA LATCH LOCATED AND INSTALLED NEW LATCHES AT #2 ENG. NACELLE STRUT AFT ACCESS DOOR PER B767-300 SRM 51-40-02-0G-0.</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

COCKPIT LIFE VEST STORAGE COMPARTMENT ABOVE 2ND OBS SEAT HAS LOOSE VELCRO.(<P>REMOVED &AMP; REPLACED DAMAGED VELCRO AT COCKPIT LIFE VEST STORAGE COMPARTMENT ABOVE SECOND OBS SEAT IAW B767 AMM 20-30-01.</P>)

Part: PIN — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

RIGHT OFF WING SLIDE INFLATION BOTTLE PIN WARNING STREAMER DAMAGED .(<P>REPLACED INFLATION CYLINDER SAFETY PIN WITH DAMAGED STREAMER ON RH WING AS REQUIRED IAW AMM 25-65-00-442-410 STEP 10.</P>)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,201 hrs · 26,218 cycles

AFT CARGO DOOR CUT OUT AFT UPPER STOP IS LOOSE(<P>SECURED STOP AT AFT CARGO DOOR CUT OUT AFT FRAME IAW B767 SRM 51-40-02</P>)

Part: WARNING MESSAGE — ILLUMINATED (ENG FIRE) · airframe 92,847 hrs · 26,143 cycles

2 HRS INTO FLIGHT RECEIVED "RT ENG FIRE" EICAS MESSAGE. RAN ALL ASSOCIATED CHECKLISTS AND SHUT RT ENG DOWN. REMOVED AND REPLACED RH ENG ASSY PER AMM 71-00-02 & W/C A-71-989-04. PRE-COOLER REPLACED AS PRECAUTION. RH & LH CORE COWLS & THRUST REVERSERS REPLACED.

Part: POWER SUPPLY — NONE · airframe 92,543 hrs · 26,079 cycles

NUMEROUS EMERGENCY LIGHTS INOP.(<P>REPLACED M736 EMERGENCY POWER SUPPLY PER B767 AMM 33-51-07-002-006. OPS CHECK GOOD.</P>)

Part: LIGHT — NONE · airframe 92,543 hrs · 26,079 cycles

NUMEROUS EMERGENCY LIGHTS INOP.(<P>RE-LAMPED EMERGENCY LIGHTS AT SEAT LOCATION16L, 28L AND 31L PER767 AMM 33-51-05-002-039. OPS CHECKED GOOD.</P>)

Part: BATTERY PACK — NONE · airframe 92,543 hrs · 26,079 cycles

NUMEROUS EMERGENCY LIGHTS INOP.(<P>REMOVED AND REPLACED POSITION M1210 BATTERY PACK PER B767 AMM 33-51-07-422-012. OPS CHECKED GOOD.</P>)

Part: BATTERY PACK — MISSING · airframe 92,347 hrs · 26,041 cycles

L1 DOOR OVERHEAD LIGHT INOP.(TRANSFERRED TO MDDR 168798 PER MEL 33-21-01-02. LP 1533523: T/S L1 DOOR OVERHEAD LIGHT INOP AND FOUND MISSING PACK AT M735. INSTALLED A NEW BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD. DMI 168798 CLOSED.</P>)

Part: LIGHT — INOPERATIVE · airframe 91,918 hrs · 25,952 cycles

L/H OUTBOARD WHITE POSITION INOP. RELAMPED LH WING REAR POSITION LT OPS CHECK OK AMM 33-43-02.</P>)

Part: LIGHT — INOPERATIVE · airframe 91,918 hrs · 25,952 cycles

EXTERIOR EMERGENCY LIGHT BY STATION 1600 L/H RELAMPED OVERWING ESCAPE LT. L645&NBSP; REPLACED COVER LENS, ENG&NBSP; LT. OPS CHECK OK PER&NBSP;</P> / <P>AMM 33-51-06</P>)

Part: STAB SYSTEM — WARNING MESSAGE · airframe 91,918 hrs · 25,952 cycles

STAB TRIM ADVISORY EICAS MESSAGE UPON LANDING. T/S FIM 27-48- F/T 809 FOUND SYSTEM OK PER AMM 27-41-00/715 E/O 6722A008CS

Part: VANE — UNSERVICEABLE · airframe 91,918 hrs · 25,952 cycles

#2 ESN 704757 HAS 1EA HPT VANE AT 5 O'CLOCK POSITION WITH CONVEX SIDE MISSING AND LIFTING MATERIAL. CONDITION IS NOT PERMITTED. REPLACED ENGINE. REMOVED #2 ENG PER B767-300 AMM 71-00-02. OK TO INSTALL SERVICIABLE ENG. / INSTALLED NEW&NBSP; SERVICIABLE ENG PER B767-300 AMM 71-00-02. OPS&NBSP; CHECK&NBSP; GOOD&NBSP; &AMP;&NBSP; NO LEAKS&NBSP;</P>)

Part: ACCESS DOOR — STUCK · airframe 91,918 hrs · 25,952 cycles

NACELLE STRUT #2 INBOARD SIDE, THE PROSV ACCESS DOOR IS LIFTED IN CLOSE POSITION. SECURED #2 ENG I/B PROSOV ACCESS DOOR IAW B767-300 SRM 51-40-02</P>)

Part: SEAL — BROKEN · airframe 91,918 hrs · 25,952 cycles

ENG. # 2 AFT NOZZLE FOUND SEVERAL FINGER SEAL BROKEN .(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; BROKEN FINGER SEAL&NBSP; AT ENG. # 2&NBSP; AFT NOZZLE AS PER 767-300 SRM 51-40-02-0G-0.</SPAN></P>)

Part: CYLINDER — OVERSERVICED · airframe 91,918 hrs · 25,952 cycles

E&E COMPARTMENT SERVICE CREW OXYGEN CYLINDER TO FULL. SERVICED CREW OXY CILINDER; AT LOWER; E&E AS PER; B767;AMM 12-15-08-603-001,35-00-00-412-005,35-11-00-206-228; 35-11-00-206-233.;ADVISORY CIRCULAR AC 43.13-1B; PAR 9-46 THRU; 9-51;PGS9-448THRU 9-459

Part: CONTROL PANEL — UNSERVICEABLE · airframe 91,918 hrs · 25,952 cycles

CAP VOR/DME TUNER CRS KNOB IS SKIPPING NUMBERS ON DISPLAY GOING FROM 120 TO 247 TO 132 AS EXAMPLES. REMOVED & REPLACED CAPT VOR CTL PANEL M91 OPS CHECK OK AMM 34-51-02.

Part: PACKING — LEAKING · airframe 91,918 hrs · 25,952 cycles

ENGINE #1, DURING PNEUMATIC LEAK CHECK, FOUND POINT L WITH LEAK REMOVED AND REPLACED PACKING &INBSP; ON LOCATION "K"&NBSP; IAW&NBSP; B767&NBSP; &NBSP;AMM&NBSP; &NBSP;20-11-00.&NBSP; &NBSP; &NBSP;NO LEAKS NOTED</SPAN></P>)

Part: FIRE SEAL — WORN · airframe 91,918 hrs · 25,952 cycles

ENG. # 2 AFT FIRE SEAL WORN OUT .(<P>REMOVED &AMP; REPLACED FIRE SEAL AT ENG. # 2 AT AFT AREANBSP; AS PER&NBSP; 767-300 SRM 51-40-02-0G-0.</P>)

Part: SENSOR — INOPERATIVE · airframe 91,918 hrs · 25,952 cycles

WHEN FUELING - AT THE REFILL PANEL, THE RESET BUTTON MUST BE HELD. - ITEM SHORT SIGNED BY FLIGHT MX - T/S PER AMM 28-55-00, FOUND ALL INDICATING POINTING TO LEFT TANK AUTO SW ASSY. REMOVED LEFT WING SURGE TANK ACCESS PANEL 542AB; IAW; REF B767 AMM 28-11-03, REMOVED AND REPLACED LT TANK FUEL LEVEL SENSOR UNIT IAW REF B767; AMM 28-21-03; OK TO CLOSE ACCESS PANEL # 542AB CLOSED LT/WING SURGE TANK ACCESS PANEL # 542AB IAW REF B767 AMM 28-11-03 3519177/KR42314M ;5/3/22 ERTS PENDING FOR OPS LEAK CHECK. CHECK LEVEL FUEL SENSOR OK AMM 28-21-04 PERFORMED LEAK CHECK NO LEAKS

Part: SAFETY CLIP — DAMAGED · airframe 91,918 hrs · 25,952 cycles

N/L/G STEERING CABLES, TURN BUCKELS HAVE SPEED TAPE ON SAFETY CLIPS ( REMOVE SPEED TAPE & REPLACE SAFETY CLIPS IF REQUIRED REMOVED & INSTALLED LOCKING CLIPS ON TURN BUCKRLS FOR NLG STEERING PER AMM 20-10-05.

Part: PACKING — LEAKING · airframe 91,918 hrs · 25,952 cycles

ENGINE #1, DURING PNEUMATIC LEAK CHECK FOUND POINT E WITH LEAK(<P>REMOVED AND REPLACED PACKING AT LOCATION&NBSP; "E"&NBSP; IAW B767 AMM&NBSP; 20-11-00. NO LEAKS NOTED.</P>)

Part: BOTTLE — OUT OF DATE · airframe 91,918 hrs · 25,952 cycles

E&;E COMPARTMENT CREW OXYGEN CYLINDER IS OUT OF DATE ,P/N 801307-00 S/N ST352350 MFG DATE 30 APR 97(REMOVED & REPLACED CREW OXYGEN BOTTLE AS PER B767-300 AMM 12-15-08. LEAK CHK GOOD AS PER&NBSP; B767-30 AMM 35-11-00-206-228..</P> / <P>&NBSP;</P>)

Part: OIL SYSTEM — OUT OF LIMITS · airframe 91,918 hrs · 25,952 cycles

DUE TO EXTENDED GROUND TIME-VISUAL INSP.OF APU OIL SERVICE IS REQUIRED. CHECK APU OIL IAW MM 12-13-04-200-801, NO OIL NEEDED

Part: SWITCH — NONE · airframe 91,918 hrs · 25,952 cycles

LEFT AND RIGHT LANDING GEAR LIGHTS INDICATIONS NOT FLUSH WITH EACH OTHER, RIGHT GEAR DOWN LIGHT HARD TO SEE ILUMINATED FROM CAPT SEAT(<P>REMOVED &AMP; REPLACED L &AMP; R L/G DIODE SUSE CARD SW. LTS &AMP; OPS&NBSP; CHECK OK AMM 33-13-00/902.</P>)

Part: AUDIO CONTROL — INOPERATIVE · airframe 91,918 hrs · 25,952 cycles

BOTH CAPT AND FO I/C , INT SWITCH ON YOKES ARE ON A DELAY WHEN COMMUNICATING, PUSH SWITCH TO TALK CANT HEAR OTHER PILOT FOR 3-5 SECOND UNTIL MIC BECOME HOT. REMOVED/REPLACED AUDIO ACCESSORY UNIT M108. TEST OK PER AMM 23-42-01

Part: JUMPER — BROKEN · airframe 91,918 hrs · 25,952 cycles

LEFT MLG EXTENSION HANDLE ACCESS DOOR # 197BL HAS THE AFT HINGE BONDING JUMPER BROKEN. REMOVED & REPLACED BONDING JUMPER&NBSP; AT LEFT EXTENSION HANDLE; ACCESS DOOR; 197BL. AFT; HINGE AND PERFORMED RESISTANCE;CHECK AND FOUND WITHIN ALLOWABLE LIMITS AS PER BOEING SWPM 20-20-00 20-20-10

Part: BLEED VALVE — DAMAGED · airframe 91,918 hrs · 25,952 cycles

APU SURGE VALVE WITH DUCT DAMAGED(<P>REMOVED AND REPLACED APU SURGE&NBSP; BLEED VALVE&NBSP; DUCT ASSY&NBSP; IAW B767-300 AMM 49-53-01. OPS CHK&NBSP; NORMAL . NO&NBSP; LEAKS FOUND .</P>)

Part: CALL CHIME — INOPERATIVE · airframe 91,918 hrs · 25,952 cycles

R4 CALL LIGHT / SOUND / CHIME REPEATLY GOING OFF-GITOST LIGHT PERFORMED PASSENGER SERVICE SYSTEM OPS CHECK. ALL CALL LIGHTS/ SOUND WORK NORMAL AS PER B767-300 AMM 23-34-00

Part: ACARS — FAULTED · airframe 91,918 hrs · 25,952 cycles

RECIEVING A DOUBLE AURAL DING WHEN REQ ACARS DATA ON RECEIVING AN ACARS/ FLIGHT PLAN MESSAGE. SHOULD ONLY BE ONE AURAL NOTIFICATION . NOT TWO. ACARS OPERATIONAL TEST OK PER B767-300 AMM 23-22-00 TLS D633T1C9

Part: SEAL — DETERIORATED · airframe 91,918 hrs · 25,952 cycles

RIGHT MLG EXTENSION HANDLE ACCESS DOOR # 198BR HAS THE INTERNAL EDGES SEAL COMING APART. REAPPLIED BLACK VINYL TAPE TO RMLG EXT HANDLE ACCESS DOOR #198BR IAW B767-300, AMM&NBSP; 20-30-01

Part: STOWAGE BOX — INOPERATIVE · airframe 91,592 hrs · 25,873 cycles

2ND OBSERVER O2 MASK TEST LEVER DOES NOT RETURN TO RESET PROPERLY.(<P>REMOVED AND REPLACED 2ND OBSERVERS O2 MASK STOWAGE BOX IAW 767 AMM 35-11-51, LEAK CHECK GOOD.</P>)

Part: BATTERY — NONE · airframe 91,364 hrs · 25,820 cycles

FUSELAGE LEFT AFT OF WINDOW 3E EMERGENCY EXTERIOR LIGHT OUT(<P>REMOVED AND REPLACED BATTERY PACK ASSY AT M738. OPS CKS GOOD IAW AMM 33-51-07.</P>)

Part: SLIDE — NONE · airframe 91,324 hrs

L1 DOOR SLIDE UNSECURE (DOOR SLIDE REMOVED LEFT IN BIF(<P>TRANSFERRED TO MDD 159678 IAW MEL CAT C, DUE DATE 20JAN22</P> / <P>12JAN22 - LP 1420099 - ITEM #19 - BWI - INSTALLED L1 DOOR LIFE RAFE ASSY PER AMM 25-66-01. OPS CHECK GOOD. THIS CLEAR DMI.</P>)

Part: NONE — NONE · airframe 91,196 hrs

IT WAS FOUND BROKEN THE SUPPORT ASSY - CARRIER P/N 141T6591-10 FROM FWD SERVICE DOOR AT CABIN PAX(<P>BROKEN PART WAS REPLACED AND TORQUE APPLIED IN ACCORDANCE WITH B767 AMM 20-11-00-910-802</P>)

Part: NONE — NONE · airframe 91,196 hrs

DENT PLUS REWORK ON FUSELAGE SKIN BETWEEN STA 282 AND STGR 19 / 20LH(<P>EVALUATED AREA PER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL III, HOWEVER IT WAS FOUND OUT OF LIMITS AND FOR SUCH REASON MXA CONTACTED TO BOEING PER SR# 3-5178994812 (LEAVE IN "AS IS" CONDITION EACH AFFECTED AREA AND RESTORE THE SURFACE FINISH)</P>)

Part: NONE — NONE · corrosion level 2 · airframe 91,196 hrs

CORROSION ON THE RH WING TRAILING EDGE FLAP, WEDGE SKIN, AND WEDGE SPAR AT OTEF STA 105.7548(<P>REPAIRED AREA IN ACCORDANCE WITH BOEING SR#3-5164623900</P> / <P>RH WING OUTBD FLAP P/N 113T3100-78 AND S/N 000889</P>)

Part: NONE — NONE · airframe 91,196 hrs

FUEL LEAK EVIDENCE ON CENTER WING AT RBL 97.42 AND STRINGER L-6(<P>FUEL LEAK WAS REPAIRED PER AMM</P>)

Part: NONE — NONE · airframe 91,196 hrs

DENT PLUS REWORK ON FUSELAGE SKIN BETWEEN STA 1540 / STA 1562 AND STGR 17 / 19LH(<P>EVALUATED AREA PER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL II AND III, HOWEVER IT WAS FOUND OUT</P> / <P>OF LIMITS AND FOR SUCH REASON MXA CONTACTED TO BOEING PER SR# 3-5175816448 (LEAVE IN "AS IS"</P> / <P>CONDITION EACH AFFECTED AREA AND RESTORE THE SURFACE FINISH)</P>)

Part: NONE — NONE · corrosion level 2 · airframe 91,196 hrs · 25,783 cycles

CORROSION ON PASSENGER CABIN CROSS FLOOR BEAM UPPER CHORD AT STA 287 BETWEEN RBL 20.0 / RBL 54.0(<P>IT WAS REPAIRED PER B767 SRM 53-00-51-2R-1 REPAIR 1 (FLOOR BEAM REPAIR)</P>)

Part: VALVE — NONE · airframe 91,196 hrs

LEAK EVIDENCE OF VALVE MODULE - NLG STEERING P/N 3790037-108(<P>VALVE WAS REPLACED IN ACCORDANCE WITH AMM 32-51-04-401-013</P>)

Part: NONE — NONE · corrosion level 2 · airframe 91,196 hrs

CORROSION ON PASSENGER CABIN CROSS FLOOR BEAM UPPER CHORD AT STA 347 AND BETWEEN RBL 20.0 TO RBL 48.0(<P>IT WAS REPAIRED PER B767 SRM 53-00-51-2R-1 REPAIR 1 (FLOOR BEAM REPAIR)</P>)

Part: FITTING — NONE · corrosion level 3 · airframe 91,196 hrs

CORROSION ON STRINGER S-38RH AND ADJACENT AREA BETWEEN STA 1562 TO STA 1582 IN BULK CARGO AREA.(<P>IT WAS REPAIRED PER B767 SRM 53-00-03-2R-2 FIGURE 201 (FLOOR BEAM REPAIR)</P> / <P>AND IT WAS REPLACED / MANUFACTURED THE END-FITTING P/N 146T0203-1 IAW MXA ENGINEERING TASK CARD NO. M6753287 (SMAL REQUEST)</P>)

Part: NONE — NONE · corrosion level 3 · 25,783 cycles

CORROSION ON STRINGER S-38LH BETWEEN STA 1562 TO STA 1582 IN BULK CARGO / AREA.(<P>IT WAS REPAIRED PER B767 SRM 53-00-03-2R-2 REPAIR 2 (FUSELAGE STRINGER REPAIR)</P>)

Part: NONE — NONE

AFTER A " PACK OFF" DEPARTURE: "FWD EQPT OVHT" EICAS. QRH COMPLETED. EQUIP COOLING PLACED IN STBY(<P>MAINTENANCE RETURNED SWITCH TO AUTO, SYSTEM OPERATES NORMAL PER B767 AMM 21-58-00.</P>)

Part: NONE — NONE

EICAS MSG "L FWD FUEL PRESS"(<P>PERFORMED OPS CHECK OF L FWD FUEL PUMP PER B767 AMM 28-21-00. SYSTEM GOOD. LIGHT EXTINGUISHED</P>)

Part: NONE — NONE · airframe 91,122 hrs · 25,761 cycles

L FWD FUEL PRESS(<P>PERFORMED OPS TEST OF L FWD FUEL PUMP. ALL CHECK OK IAW AMM 28-21-00. OK FOR SERVICE.</P>)

Part: VALVE — NONE · airframe 91,114 hrs · 25,759 cycles

LEFT ENGINE ANTI-ICE VALVE DISAGREEMENT LIGHT. CYCLE TO CLEAR.(<P>REMOVED &AMP; REPLACED LEFT ENGINE INLET TAI VALVE IAW AMM 30-21-03. OPS CHECKED &AMP; LEAK CHECKED GOOD.</P>)

Part: NONE — NONE · 25,751 cycles

LEFT FORWARD FUEL PUMP(<P>LEFT FWD FUEL PUMP OPS CK NORMAL PER AMM 28-42-00. ACFT OK FOR SERVICE.</P>)

Part: NONE — NONE

"R AFT FUEL PUMP" EICAS MESSAGE IN CRUISE FLIGHT.(<P>R AFT FUEL PUMP C/B RESET IAW AMM 20-60-01. NO FAULS NOTED &AMP; R AFT PUMP OPS CHECK SATISFACTORY IAW AMM 28-22-03.</P>)

Part: NONE — NONE

APU FAULT UPON ENGINE SHUTDOWN. RESTART NOT SUCCESSFUL.(<P>PERFORMED BITE ON APU ECU-FAULTED, RESET ECU, APU STARTED NORMALLY PER AMM 49-61-05.</P>)

Part: FILTER — NONE

ON INITIAL ROTATION AND CLIMBOUT AND DURING CRUISE CLIMB FL330 TO FL350 WE RECEIVED EICAS MESSAGE R ENG FUEL FILT(<P>REMOVED AND REPLACED RH ENG FUEL FILTER ASSY IAW PER MM 73-11-03. OPS &AMP; LEAK CHK OK.</P>)

Part: PUMP — FALSE INDICATION (L FWD)

L FWD FUEL PUMP EICAS MSG ON FINAL APPROACH L FWD FUEL PUMP CK NORMAL PER AMM 28-42-00. A/C OK FOR SERVICE.

Part: TRANSMITTER — FAILED

FIXED ELT FAILS GPS TEST. TRANSFERRED TO MDDR 154060, DDG 25-23-10-02C, CAT D. MAINT ACTIONS COMPLETED. DUE 22 JAN 22 PLACARD INSTALLED.&NBSP; 30SEP21 - LP 1314601 - ITEM 8 -&NBSP; IAH - REMOVED AND REPLACED FIX ELT. IAW AMM 25-63-03. OPS CHECK NORMAL. THIS CLEARS MDDR #154060. PLACARD REMOVED. LC@0050Z

Part: APU — FAILED

APU FAULT, 3 ATTEMPTS TO START UNSUCCESSFUL APU ECU INTERROGATED AND NO FAULTS. APU SUCCESSFULLY STARTED IAW AMM 49-11-00. OK FOR SERVICE.

Part: PUMP — FALSE INDICATION · 25,709 cycles

LEFT FWD FUEL PUMP EICAS.(<P>PERFORMED OPS CK OF LT FWD FUEL PUMP ALL CHECKS OK NO MSG OR FAULTS PER AMM 28-42-01</P>)

Part: APU — FAULT MESSAGE

APU FAULT, 3 ATTEMPTS ON GROUND.(<P>STARTED APU ON FIRST TRY - OIL QTY READING 0.50 - APU OPS CKS OK PER AMM 49-41-00</P>)

Part: EXHAUST FAN — FALSE INDICATION

STATUS MSG AFT EQ EXH FAN 1(<P>CLEARED MSG PER AMM 21-58-00.</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 90,800 hrs · 25,693 cycles

RADAR RETURNS VERY WEAK. NEED MAX GAIN TO SEE WX RETURNS.(<P>PERFORMED FIM TASK 34-43 FAULT TREE 805 AND WEATHER RADAR OPS CHECK IAW AMM 34-43-00. OPERATIONAL CHECK OK AT THIS TIME.</P>)

Part: PLACARD — DAMAGED (COCKPIT) · airframe 90,723 hrs · 25,675 cycles

COCKPIT L/H AND R/H WINDOW PLACARD " WINDOW NOT CLOSED " DAMAGED. REMOVED AND REPLACED THE DAMAGED PLACARD IAW AMM 20-10-12-004-001 AND 20-10-12-404-004.

Part: CHIP DETECTOR — LEAKING (APU OIL SYS) · airframe 90,723 hrs · 25,675 cycles

APU LEAKING OIL FROM THE MAGNETIC CHIP DETECTOR FOR THE GEAR BOX. REMOVED AND REPLACED DRAIN PLUG MAGNETIC DRAIN PLUG,TORQUED TO SPECS AS PER AMM 20-11-00 & LEAK CHECKED GOOD.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 90,723 hrs · 25,675 cycles

COCKPIT CAPTAIN SMOKE GOOGLES LENS DAMAGED P/N MXP210-00. REMOVED & REPLACED THE CAPT. SMOKE GOOGLES IAW LOPA AND AMM 25-64-00.

Part: DIRECTOR — FAULTED (FLT DIRECTOR) · airframe 90,723 hrs · 25,675 cycles

INSTR SOURCE SELECTOR FLT DIR CAPT "C" FD "C" FOR BOTH FLT DIR PITCH UP. PERFORMED OPERATIONAL TEST OK PER AMM 22-10-00/715 REV 101/133. PERFORMED MCDP GND TEST L/O AUTO LAND OK PER AMM 72-03 F/T 820.

Part: FAULT LIGHT — FALSE ACTIVATION (APU)

APU FAULT 3 FAILED ATTEMPTS(<P>PERFORMED OPERATIONAL CHECK OF APU ALL CHECKS OK. NO FAULT NOTED B767 AMM 49-11-00.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 90,681 hrs

STATUS MSG R ENG ANALOG N2(<P>PERFORMED FIM 73-21 FAULT TREE 901. NO DEFECTS FOUND.</P>)

Part: OIL SYSTEM — LOW (APU)

UNABLE TO START APU, "APU FAULT". SERVICED APU TO CORRECT LIMITS IAW AMM 12-13-04 AND OPS CK OF APU GOOD AT THIS TIME IAW AMM 49-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG N2)

STATUS MSG R ENG ANALOG N2(<P>T/S PER FIM 77-12 TREE 809, MSG CLEARS. NO FAULTS NOTED. SYS OK FOR SVC.</P>)

Part: APU — FAULTED

APU FAULT - 3 ATTEMPTS(<P>APU STARTS NORMAL AFTER 30 MIN ON AND PER MM 49-11-01</P>)

Part: APU — FAULTED

AFTER LANDING, APU FAULT EICAS MESSAGE DURING APU START ATTEMPT. ATTEMPTED 3 STARTS; APU ACCELERATED TO 23% AND THEN SHUTDOWN ON EACH ATTEMPT.(<P>PERFORMED BITE ON ECU, NO FAULTS. STARTED APU FIRST TRY PER AMM 49-50-00. APU OK FOR SERVICE.</P>)

Part: DUCT — LEAKING (ACM)

LT BLD DUCT LEAK(ON GND APU PWR &AMP; AIR).(<P>FOUND COUPLING TO ACM LOOSE, ADJUSTED SAME PER AMM 21-51-00, LEAK CKS GOOD.</P> / <P>16JUL21 - 1476169 - ITEM# 3 - BWI - ADJUSTED LOWER REAR COUPLING TO ACM PER 767 AMM 21-51-00. LEAK CHECK GOOD AT THIS TIME. NO MSGS. DUCT PRESSURE RISE IS OK.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 90,390 hrs · 25,609 cycles

FWD EQPT OVHT ON T/O. RAN QRH, COOLED DOWN. EICAS CLEARED.(<P>T/S PER FIM 21-58 TREE 909, NO FAULTS NOTED. SYSTEM CHECK OK. AMM 21-58-00.</P>)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · 25,604 cycles

2 BATTERY PACKS &AMP; 2 BATTERY CHARGERS REMOVED FROM LEFT OVERWING TO ACFT 480(<P>FWD TO MDDR 149803 PER MEL 33-51-01C, CAT C, DUE 17JUL21, PLACARD INSTALLED.</P> / <P>09JUL21 - LP 1476142 - ITEM 14 - IAH - REMOVED AND REPLACED 1EA BATTERY CHARGER AND BATTERY IAW AMM 33-51-00. BOTH BATTERY AND CHARGER CHANGED ONLY. OPS CHECKS OK. THIS CLOSES MDDR 149803.</P> / <P>LP1484180 ITEM# 9 - REMOVED AND REPLACED 1EA BATTERY CHARGER AND BATTERY IAW AMM 33-51-00. BOTH BATTERY AND CHARGER CHANGED ONLY. OPS CHECKS OK.&NBSP;</P>)

Part: LENS — DETACHED (EMERGENCY LIGHT)

12H OVHD EMERGENCY LIGHT LENS WILL NOT STAY ON.(<P>RESCURED 12H OVHD EMERGENCY LIGHT LENS IAW 33-51-00. OPS CKS GOOD.</P>)

Part: A/C PACK — ODOR

BURNING SMELL COMING FROM PACKS, INSP RAM AIR INTAKE TO HEAT EXCHANGERS.(<P>INSPECTED LEFT AND RIGHT RAM AIR INTAKE TO HEAT EXCHANGER, NO DEBRIS FOUND. NO BLOCKAGE REF AMM 36-11-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 90,325 hrs · 25,596 cycles

"R ENG PRV" STATUS MSG(<P>C/W FIM 36-10 TREE 847, INSP OF PRV AND BITE OF AIR SUPPLY MODULE NO FAULTS FOUND, A/C OK FOR SERVICE.</P>)

Part: OIL COOLER — MALFUNCTIONED (APU) · airframe 90,291 hrs

LOW APU DUCT PRESSURE DURING START DUE TO HIGH EGT.(<P>APU PNEUM. PLACED ON MEL 49-11-01-01 CAT C DEFRRAL # 149299. RS 1437.</P> / <P>27JUN21 LP 1402166 ITEM 3: REMOVED AND REPLACED APU AIR/OIL COOLER IAW B767 AMM 49-27-00. PERFORMED LEAK AND OPS CHECKS/LEAK CHECK WITH NO DEFECTS NOTED IAW B767 AMM 49-00-00. THIS CLEARS DEFERRAL 149299. MCC NOTIFIED.</P>)

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 90,277 hrs · 25,582 cycles

RT PACK INOP. FWD TO MDDR 148438 PER MEL 21-51-01-01. CAT C, DUE 22JUN21, PLACARD INSTALLED. DISP: RS @ 13:19Z. OPS CHK. REACTIVATED RT PACK FOR MTC CONVENIENCE OF TROUBLEHOOTING PER AMM 21-48-00. THIS CLEARS MDDR 148438. PLACARD REMOVED. DISP: RKB @ 1533Z</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 90,277 hrs

BURNING SMELL IN CABIN ON DEPARTURE.(<P>ACCOMPLISHED FUMES IN CABIN CONDITIONAL INSPECTION AMM 05-51-56-202-001, NO FAULTS FOUND. OK FOR FURTHER SERVICE.</P>)

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 90,275 hrs · 25,581 cycles

AT FL 410 WEATHER RADAR DID NOT PAINT WEATHER ON L/R(<P>PERFORMED WX RADAR BITE FOR LEFT AND RIGHT SYSTEM PER FIM 34-43 FLT 805, NO FAULTS, TEST GOOD BOTH LT AND RT WX RADAR<BR /></P>)

Part: CLAMP — LEAKING (APU SURGE) · airframe 90,275 hrs · 25,581 cycles

APU AIR DROPS TO 5 PSI DURING ENGINE START/ SLOWLY RECOVERS. TESTED NEW ENG VALVE, AMM 49-53-07, NO HELP, REINSTALLED ORIGINAL VALVE ASSY. INSTALLED APU SURGE CONTROLER VALVE HOSE CLAMP IAW AMM 49-53-01. PERFORMED OPS CHECK ON THE APU SURGE VALVE PER AMM 49-11-00. MAX PRESSURE 12 PSI ORIGINAL SURGE VALVE RE-INSTALLED.

Part: SWITCH — FAILED · airframe 90,275 hrs · 25,581 cycles

BOTH PACK CONTROLLERS ARE FAULTING THE ALTITUDE SW(<P>REMOVED AND REPLACED PACK CONTROL ALTITUDE SWITCH IAW AMM 21-51-17, PERFORMED BITE TEST ON PACK TEMP CONTROLLER PER TASK 21-51-14-705-035, OPS TEST GGOD. NO OTHER DEFECTS NOTED AT THIS TIME<BR /></P>)

Part: ACTUATOR — FAULTED (BLEED) · airframe 90,240 hrs · 25,571 cycles

APU BLEED AIR MAX 12 PSI, TOO LOW FOR ENGINE START(<P>FWD TO MDDR #148250 PER MEL 49-11-01-01, CAT C, DUE 18 JUN 21. PLACARD INSTALLED. REMOVED AND REPLACED ECU, NO HELP. REMOVED AND REPLACED SURGE VLV. NO HELP. INSPECTED SURGE VLV SENSE LINE AND IGV FREE PLAY PER FIM 49-11 TREE 980 IGV CONNECTOR STILL LOOSE. REMOVED AND REPLACED IGV ACTUATOR REF AMM 49-52-02, OPS CK FAIL. REMAINS OPEN FOR FURTHER T/S.</P><P>LP 1484183: INSPECTED AND FOUND INLET CLOGGED WITH CICADAS. CLEANED CICADAS AND OPS CK APU. APU AND ALL INDICATIONS GOOD AT THIS TIME IAW AMM 49-11-00. THIS CLEARS DMI 148250. PLAC REMOVED.</P>)

Part: VALVE — NO TEST (LT ENGINE FUEL) · airframe 90,240 hrs · 25,571 cycles

L ENG SPAR VALVE CHECK FAILED ON START(<P>NOTED BY MAINTENANCE. ENGINE SHUTDOWN AFTER COOL DOWN, L ENG RESTARTED IAW AMM 71-00-00. ALL IND NORMAL, OK FOR SERVICE.

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 90,240 hrs · 25,571 cycles

R/H START VALVE TRANSIT LIGHT DOES NOT EXTINGUISH IN OPEN POSITION.(<P>REMOVED AND REPLACED&NBSP;#2 ENGINE VALVE ENGINE STARTER IAW 767 AMM 80-11-02-404-017-H00. REQUIRES OPS CHECK ON ITEM 13. LP 1476181.</P><P>LP 1476181, ITEM M13: C/W ENG STARTER OPS CK. OK PER AMM 80-11-02</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 90,192 hrs · 25,561 cycles

L FWD FUEL PUMP EICAS MESSAGE ON TAXI.(<P>MSG SELF CLEARED AFTER PARKING AT THE GATE. SYSTEM CK GOOD. ACFT OK FOR SVC PER AMM 28-42-01</P>)

Part: PUMP — LOW PRESSURE (LT HYD SYSTEM) · airframe 90,181 hrs

ITEM#1 - L HYD QTY EICAS MSG IN FLIGHT. ITEM# 2 - L HYD PRIME PUMP EICAS MSG IN FLIGHT. TURNED PUMP OFF PER QRH. ITEM# 3 - L HYD SYS PRESSURE EICAS/ ALL LEFT HYD PUMPS OFF.(<P>ITEM #1 &AMP; #3 CORRECTIVE ACTION - LOG# 1092013 - ITEM# 6 - SOF - 31MAY21 - POPPET INDICATOR REMOVED, INSPECTED AND RESEATED IAW AMM 29-11-15. LEAK CHK CARRIED OUT. NO LEAKS EVIDENT.</P><P>ITEM# 2 CORRECTIVE ACTION - LOG# 1092013 - ITEM# 2 - SOF - 31MAY21 - AFTER ENGINE RUN LEAK CHECK, FOUND HYD LEAK AT L/H ENG EDP. REMOVED &AMP; REPLACED EDP IAW AMM 29-11-05 OPN CHK SATIS. NO FURTHER LEAKS EVIDENT.</P>)

Part: LATCH — LOOSE (STRUT DOOR) · airframe 90,133 hrs · 25,545 cycles

# 1 ENGINE STRUT DOOR PANELS LATCHES FOUND LOOSE(<P>REMOVED AND REPLACED&NBSP; DAMAGED LATCHES AT # 1 ENG STRUT DOOR PANELS I/B&NBSP; AND O/B&NBSP; PER&NBSP; B767-300</P><P>AMM&NBSP; &NBSP;20-11-00-910-802</P>)

Part: CONTAINMENT BAG — DAMAGED (FWD BIN) · airframe 90,133 hrs · 25,545 cycles

FWD OVHD BIN AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN . P/N AS-002-1(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AT&NBSP; FWD&NBSP; OVHD BIN&NBSP; AS PER&NBSP; B767-300</P><P>AMM&NBSP; &NBSP;25-60-00</P>)

Part: GASKET — LEAKING (NR 2 FUEL PUMP) · airframe 90,133 hrs · 25,545 cycles

#2 ENG. FUEL PUMP LEAKING DURING WET MOTORING. REMOVED & REPLACED #2 ENG FUEL PUMP GASKET IAW AMM 79-21-01 REV&NBSP; 132&NBSP; PENDING FOR LEAK CHECK. LEAK CHECK ACCOMPLISHED PER 71-00-00-712-168-M03-N0, NO LEAKS NOTED.

Part: SUPPORT BRACKET — DAMAGED (RT AFT PBE) · airframe 90,133 hrs · 25,545 cycles

MAIN CABIN AFT R/H PBE SUPPORT BRACKET DAMAGED. P/N AC4036-1(<P>REMOVED AND REPLACED DAMAGED BRACKET AT MAIN CABIN AFT R/H&NBSP; PBE PER&NBSP; &NBSP;B767-300</P><P>AMM&NBSP; &NBSP;20-11-00-910-802 .</P>)

Part: ROD — DAMAGED (NR 1 NACELLE) · airframe 90,133 hrs · 25,545 cycles

# 1 ENGINE O/B CORE COWL OPEN HOLD ROD IS DAMAGED .(<P>REMOVED &AMP; REPLACED #1 ENG O/B CORE COWL HOLD OPEN ROD PER AMM 70-50-00.</P><P>OPS CHECK GOOD</P>)

Part: RUB STRIP — DAMAGED (NR 2 NACELLE) · airframe 90,133 hrs · 25,545 cycles

# 2 ENG. CORE COWL RUB STRIP 9 O' CLOCK POSITION 1EA RIVET MISSING IAW 78-11-00.(<P>REMOVED AND REPLACED WORN RUB STRIP AND DAMAGED SCREW AT #2 ENG CORE COWL BY 9 O'CLOCK POSITION PER AMM 20-11-00-910-802.

Part: MESH — MISSING (THRUST REVERSER) · airframe 90,133 hrs · 25,545 cycles

LEFT ENG. LH REV. MESH 9-11 O' CLOCK MISSING IAW EO6778A019 PART 1 C/W PART 2 DUE NEXT A CHECK .(<P>REMOVED #1 ENG OUTBD TRANSLATING COWL TO ACCESS AND RETAIN&NBSP; IAW&NBSP; AMM&NBSP; 78-31-10-004-001-H00</P><P>REV 101.</P><P>ACCOMPLISHED PERMANENT REPAIR&NBSP; AT&NBSP; L/H ENG I/B&NBSP; T/R&NBSP; PER&NBSP; ATLAS&NBSP; AIR&NBSP; &NBSP;EO&NBSP; 6778A019&NBSP; REV 4&NBSP;</P><P>REPAIR&NBSP; ACCOMPLISHED PER AVENIR AVIATION&NBSP; &NBSP;FAA&NBSP; # 8AVR479B&NBSP; &NBSP; R.O 5002563&NBSP; &NBSP;AND&NBSP; WO&NBSP; W15623</P><P>CMM&NBSP; 78-32-02&NBSP; REV 61&NBSP; &NBSP;8130&NBSP; ATTACHED FOR TRANSLATING&NBSP; COWL&NBSP; INSTALLATION&NBSP; SEE&NBSP;&NBSP;</P><P>NON ROUTINE #49</P>)

Part: TRANSMITTER — LEAKING (NR 2 ENG FUEL) · airframe 90,133 hrs · 25,545 cycles

#2 ENG FUEL TRANSMITTER LEAKING DURING WET MOTORING(<P>REMOVED AND REPLACED ENGINE FUEL PUMP INTERSTAGE&NBSP; PRESSURE TRANSMITTER IN ACCORDANCE&NBSP; WITH&NBSP;B767&NBSP; AMM&NBSP; REMOVAL-&NBSP; &NBSP;73-33-01-002-001-H00 INSTALLATION- 73-33-01-402-007-H00.</P><P>REQUIRES LEAK&NBSP; AND OPS CHECK ACCOMPLISHED&NBSP; P.P&NBSP; TEST&NBSP; #2&NBSP; ( DRY MOTOR) REF MM&NBSP;&NBSP;</P><P>71-00-00-712-168-H05&NBSP; NO LEAKS&NBSP; NOTED</P>)

Part: CONTAINMENT BAG — FAILED (AT BIN) · airframe 90,133 hrs · 25,545 cycles

AFT R/H OVHD BIN AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN P/N AS-002-1.(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AFT R/H BIN AS PER&NBSP; B767-300&NBSP; AMM 25-60-00<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIP OVRHT) · airframe 90,133 hrs · 25,545 cycles

FWD EQPT OVHT EICAS MESSAGE ON INITIAL CLIMB OUT FOLLOWED QRH, CONTINUED FLIGHT WITH EICAS MESSAGE EXTINGUISHED AFTER HAVING TO GO BACK TO AUTO AFTER 30 MIN(<P>OPS TEST OF EQUIPMENT COOLING SYSTEM CARRIED OUT IAW AMM 21-58-00. ALL TEST PASS, OK FOR SERVICE</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 90,133 hrs · 25,545 cycles

L FWD FUEL PUMP EICAS MESSAGE ON DESCENT FOLLOW QRH, CONTINUED FLIGHT(<P>L FWD FUEL PUMP MSGS ERASED AFTER PARKING AT GATE. ALL INDICATION NORMAL OK FOR SERVICE, AMM 28-42-01</P>)

Part: PRESSURE SWITCH — FAULTED (LT FUEL PUMP) · airframe 90,100 hrs · 25,539 cycles

"L FWR FUEL PUMP" EICAS ADVISORY. REPEAT WRITE UP.(<P>REMOVED AND REPLACED&NBSP;LT FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECK AND LEAK TEST GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 90,100 hrs · 25,539 cycles

L FWD FUEL INOP EICAS ADVISORY.(<P>L FWD FUEL PUMP OPS CHECK GOOD PER M/M 28-22-00, SYSTEM CHECK OK FOR CONTINUED SERVICE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 90,085 hrs · 25,534 cycles

LEFT FWD FUEL PUMP EICAS MSG ON DESCENT W ASSOCIATED PRESS LIGHT(<P>LEFT FWD FUEL PUMP - OPS CK OK PER AMM 28-22-00 SYS OK FOR SERVICE.</P>)

Part: RELAY — FAILED (LT IDG) · airframe 90,050 hrs · 25,527 cycles

L IDG VALVE STATUS MSG. T/S PER FIM 24-20 FT 802 - FOUND L IDG VALVE FAILURE RELAY 9K468 BAD, REMOVED AND REPLACED PER WDM 24-11-11. OPS TEST GOOD IAW AMM 24-11-00</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT IDG VALVE) · airframe 90,050 hrs · 25,527 cycles

STATUS MESSAGE " L IDG VALVE" DISPLAYED. PERFORMED BITE TEST OF THE BPCU IAW FIM 24-20FT807 NO FAULTS REMAIN AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT IDG VALVE) · airframe 90,050 hrs · 25,527 cycles

L IDG VALVE MESSAGE. PERFORM BITE TEST OF THE BPCU AND NO FAULT AT THIS TIME, FAULT MSG CLEARED.

Part: PUMP — FAULTED (LT FUEL BOOST) · airframe 89,990 hrs · 25,515 cycles

L FWD FUEL PUMP CAUTION ILLUMINATED AFTER LANDING(<P>R&AMP;R L FWD FUEL BOOST PUMP IAW AMM 28-22-03, OPS TEST GOOD<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 89,960 hrs · 25,509 cycles

RIGHT AFT FUEL PUMP EICAS ADVISORY MSG(<P>OPS CHECK OF RIGHT AFT FUEL PUMP CARRIED OUT IAW AMM 28-22-01. OPS CHECK SATIS. OK FOR SERVICE<BR /></P>)

Part: VALVE — MALFUNCTIONED · airframe 89,946 hrs · 25,506 cycles

FWD EQUIP VAL EICAS ADVISORY REPEAT WRITE UP.(<P>TRANSFERRED TO DMI 145549 IAW DDG 21-58-07-02-01 PROCEDURE 2 CARRIED OUT, CAT C, STR 0346Z</P><P>BWI MX, LP 1335298, ITEM M3: REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05, OPS TEST GOOD. DMI CLEARED. PLACARDS REMOVED. DISP TJ @ 1028Z</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIP BAY) · airframe 89,946 hrs · 25,506 cycles

FWD EQUIP EICAS ADVISORY(<P>FIM 21-58 TASK 805 CARRIED OUT. MSG ERASED. OK FOR SERVICE.</P>)

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 89,936 hrs · 25,504 cycles

LEFT FWD FUEL PUMP EICAS MSG ON FINAL(<P>TRANSFERRED TO MDDR 145506 IAW MEL 28-22-01, CAT C.</P><P>REMOVED AND REPLACED FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS AND LEAK CHECKS GOOD. THIS CLEARS MDDR 145506. MCC NOTIFIED. PLACARDS REMOVED. CW 23:54Z</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT IDG VALVE) · airframe 89,890 hrs · 25,494 cycles

STATUS MSG L IDG VALVE(<P>INSPECTED L IDG OIL LEVEL AND DELTA "P" IAW B767AMM 12-13-03. NO DEFECTS NOTED. MESSAGE CLEARED.</P>)

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 89,910 hrs · 25,500 cycles

L GEN OFF EICAS MESSAGE AFTER START.(<P>TRANSFERRED TO MDDR 145429, CAT B, DUE DATE 19APR21. MEL 24-00-01-01.</P><P>19APR21 - LP 1335294 - ITEM# M8 - BWI - REPLACED L/H GEN IAW AMM 24-11-01. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS MDDR # 145429. MCC NOTIFIED. PLACARD REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 89,946 hrs · 25,506 cycles

EICAS MSG L FWD FUEL PUMP.(<P>CONTROL ALL BREAKERS ARE CLOSED AND NO CURRENT EICAS MSG. NO DEFECTS NOTED AT THIS TIME IAW AMM 28-22-00.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG A/ VALVE) · airframe 89,800 hrs

STATUS MESSAGE: L ENG TAI VALVE(<P>R/R ENG INLET TAI VALVE LH IAW AMM 30-21-03. PERFORMED OPS CHECK, OPS CHECK GOOD.</P>)

Part: ANTI-ICE VALVE — FAILED (ENGINE) · airframe 89,815 hrs

STATUS MESSAGE: L ENG TAI VALVE(<P>R/R ENG INLET TAI VALVE LH IAW AMM 30-21-03. PERFORMED OPS CHECK. OPS CHECKS GOOD</P>)

Part: CIRCUIT CARD — FAULTED (RT A/C PACK) · airframe 89,782 hrs · 25,471 cycles

NO EICAS MSG WHEN RT PACK SW OFF(<P>REMOVED AND REPLACED RT PACK FLOW CIRCUIT CARD PER AMM 21-51-09 TASK 401. OPS CKS GOOD AND THIS CLEARS MDDR 144783.</P>)

Part: PUMP — FAILED (LT FUEL) · airframe 89,709 hrs · 25,453 cycles

L FWD FUEL PUMP FAIL AFTER LANDING(<P>L FWD FUEL PUMP OPS CHK SATIS. NO ACTIVE MSGS. OK FOR SERVICE. IAW AMM 28-22-00.</P>)

Part: ROD — INOPERATIVE (NACELLE DOOR) · airframe 89,654 hrs · 25,440 cycles

LEFT ENGINE HOLD ROD INOP. REMOVED AND REPLACED NR 1 ENG INBD AFT HOLD OPEN FAN COWL ROD IAW B767 AMM 71-11-11. OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,651 hrs · 25,438 cycles

AISLE EMERGENCY LIGHT OUT AT SEAT # 25HK - REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP, OPS CHECKS GOOD IAW AMM 33-51-05.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 89,651 hrs · 25,438 cycles

EMERGENCY (AISLE) LIGHTS OUT FROM SEAT # 1AC-10AC DURING TEST. REMOVED AND REPLACED BATTERY POWER SUPPLY M735, OPS CHECKS GOOD IAW AMM 33-51-07.

Part: RELAY — FAILED (LT FUEL PUMP) · airframe 89,650 hrs · 25,437 cycles

LEFT FWD FUEL PUMP EICAS. TRANSFER TO DDG CONTROL MEL 28-22-01, MDDR 142605, CAT "C", DUE 28FEB21 20FEB21 - LP 1273119 - ITEM NR 3 - BWI. REMOVED AND REPLACED K10703 IAW AMM 28-22-18. THIS CLEARS MDDR 142605. 1955 JT

Part: HOOK AND LOOP — UNSERVICEABLE (GLARESHIELD) · airframe 89,610 hrs · 25,429 cycles

EVAS GLARESHIELD VELCRO UNSERVICEABLE (LEFT) CAPT. SIDE(<P>TRANSFERRED TO MDDR #142055 PER MEL 25-63-06, CAT D, DUE 06 JUN 21.</P><P>LP&NBSP;1273095: INSTALLED CAPTAIN'S CSVS VELCRO IAW SMM 25-60-99. THIS CLEARS MDDR 142055.</P>)

Part: CIRCUIT BREAKER — POPPED (DOOR ACTUATOR) · airframe 89,563 hrs · 25,417 cycles

APU FAILED TO START UPON ARRIVAL, 3 ATTEMPTS. DOOR ACTUATOR CB FOUND POPPED, CB RESET IAW AMM 20-60-01. OPS CHK SATISFACTORY. APU START FIRST ATTEMPT.

Part: INDICATOR — WARNING MESSAGE (APU BAY) · airframe 89,563 hrs · 25,417 cycles

STATUS MESSAGE APU OIL QTY, VISUALLY VERIFIED APU OIL QT. SERVICED WITH 1/4 OF A QUART. APU OIL LVL OK PER AMM 12-13-04.

Part: VALVE — INOPERATIVE (CABIN TEMP TRIM) · airframe 89,521 hrs · 25,408 cycles

FORWARD ZONE CABIN TEMP TRIM AIR VALVE INOPERATIVE. FWD CABIN AIR CONDITIONING ZONE INOP LIGHT. TRANSFERRED TO DMI 141569, IAW MEL 21-61-04-01B CAT C DUE 07FEB21. MCC NOTIFIED, PLACARDS INSTALLED. LOG PAGE 1273154: REPLACED TRIM VALVE MODULATING IAW AMM 21-61-07. OPS AND LEAK CHECK GOOD. THIS CLEARS DMI 141569. MCC NOTIFIED.

Part: SHUTOFF VALVE — INTERMITTENT (APU) · airframe 89,508 hrs · 25,405 cycles

APU BLEED AIR S/O VALVE OPERATIONS INTERMITTENTLY. REMOVED AND REPLACED APU BLEED AIR S/O VALVE, IAW AMM 36-11-10, OPERATIONS CHECK OK.

Part: TRIGGER — MISINSTALLED (SLIDE CYLINDER) · airframe 89,474 hrs · 25,396 cycles

LEFT OFF WING ESCPAE INFLATION CYLINDER WHITE INDICATOR NOT VISIBLE AND INFLATION TRIGGER CABLE NOT INSTALLED CORRECTLY. REMOVED AND REPLACED LEFT OFF WING ESCAPE INFLATION CYLINDER, AS PER B767 AMM 25-65-02.

Part: ANTI-ICE VALVE — STUCK (RT ENGINE) · airframe 89,472 hrs · 25,395 cycles

RT ENGINE A/I VALVE INTERMITTENTLY STICKS WHEN OPERATING. REMOVED AND REPLACED RT ENGINE COWL ANTI ICE VALVE, IAW AMM 30-21-03. PERFORMED OPERATIONS TEST AND LEAK CHECK, FOUND GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 89,443 hrs · 25,389 cycles

SEAT NR 8HC AISLE EMERGENCY LIGHT LENS MISSING. INSTALLED AISLE EMERGENCY LIGHT LENS, IAW AMM 33-51-05.

Part: CONTROLLER — MALFUNCTIONED (FWD CABIN TEMP) · airframe 89,376 hrs · 25,371 cycles

FWD CABIN TEMP CONTROLLER INOPERABLE. CABIN COMPARTMENT TEMP CONTROL SYSTEMS, PASSENGERS, -200/300/-400. PERFORMED BITE CHECK ON CABIN TEMP CONTROLLER, RESET CB INOPERABLE, CLEARED. OPERATIONS CHECK GOOD, PER 767 FIM 31-61-FT 803.

Part: TRANSMITTER — ERRATIC (APU OIL QTY) · airframe 89,323 hrs · 25,360 cycles

APU OIL QTY IND. INTERMITTENT/ERRATIC. REMOVED AND REPLACED APU OIL TRANSMITTER, PER AMM 49-94-04. OPERATIONS CHECK OK.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 89,280 hrs · 25,349 cycles

LT FWD FUEL PRESSURE LIGHT. REMOVED AND REPLACED LEFT FWD BOOST PUMP 28-22-03. OPERATIONS AND LEAK CHECK NORMAL.

Part: PRESSURE SWITCH — MALFUNCTIONED (BOOST PUMP) · airframe 89,247 hrs · 25,341 cycles

LEFT FWD BOOST PUMP HAS INTERMITTENT PRESSURE LIGHT WHEN OPERATING. REMOVED AND REPLACED LEFT FWD BOOST PUMP PRESSURE SWITCH, IAW AMM 28-42-01. OPERATIONS AND LEAK CHECKS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG ANTI ICE) · airframe 89,236 hrs · 25,339 cycles

RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED. OPERATIONS CHECK, IAW 30-21-03, NO DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (AFT GALLEY) · airframe 89,225 hrs · 25,337 cycles

AFT GALLEY EMERGENCY FLASHLIGHT ASSEMBLY RED LIGHT NOT FLASHING. REMOVED AND REPLACED AFT GALLLEY EMERGENCY FLASHLIGHT, IAW AMM 25-60-00.

Part: PUMP — INOPERATIVE (LT FUEL) · airframe 89,178 hrs · 25,328 cycles

LEFT FWD FUEL PUMP INOPERABLE. TRANSFERRED TO MDDR 137978, IAW MEL 28-42-01-01 CAT "C" DUE 27NOV20. VERIFIED OPERATION OF FUEL SYSTEM, PER DDG 28-42-01-01. OPERATIONS CHECK GOOD AT THIS TIME, NEXT INSPECTION DUE EVERY FLIGHT DAY. 18NOV20/1272892/ITEM-M2/RMS. REMOVED AND REINSTALLED AFTER CLEANING PRESS SWITCH, IAW B767 28-42-01, THIS CLEARS MDDR 137978.

Part: MODULATING VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 89,164 hrs · 25,324 cycles

FWD CABIN TEMP EICAS MESSAGE ILLUMINATED PRIOR TO BLOCKOUT(<P>TRANSFERRED TO MDDR #137963 IAW DDG MEL# 21-61-01-01, CAT C, DUE ON 27NOV20. DISPATCH: C.W. @ 0050Z.<BR /></P><P>22NOV20, LP 1272907 M4 - BWI - REMOVED AND REPLACED FWD ZONE TRIM AIR MODULATING VALVE. IAW AMM 21-61-07. OPS CHECK GOOD. THIS CLEARS MDDR #137963. MCC NOTIFIED. PLACARD REMOVED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 89,087 hrs · 25,305 cycles

LT ENGINE TAI STATUS MESSAGE. T/S IAW B767 FIM 30-21 FAULT TREE 805. NO FAULTS FOUND AT THIS TIME. STATUS MESSAGE CLEARED. MCC NOTIFIED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 88,896 hrs · 25,264 cycles

LEFT FWD FUEL PUMP EICAS ON SHORT FINAL. CHECKED PRESSURE SWITCH AND CONNECTOR. OPERATIONS AND INDICATION OF FWD FUEL PUMP OK, PER MM 28-42-01 AND FIM 28-22 FAULT TREE 827.

Part: VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 88,868 hrs · 25,259 cycles

FWD CAB TEMP EICAS MESSAGE, COMPT TEMP INOPERABLE LIGHTS, PASSENGER, -200/-300, TRIM AIR MODULATING VALVE CLOSED. TRANSFERRED TO MDDR 136025, IAW MEL 21-61-06-01-01A, CAT C. REMOVED AND REPLACED FWD CABIN TRIM AIR VALVE ASSEMBLY, PER AMM 21-67-07. OPERATIONS CHECKS GOOD. THIS CLEARS MDDR 136025. DISP SP AT 2017.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 88,868 hrs · 25,259 cycles

AFTER LEVEL OFF LT ENGINE HPSOV EICAS STATUS. COMPLETED CHECK LIST. RAN BITE CHECK ON AIR SUPPLY MODULE, PER AMM 36-23-00, NO FAULTS NOTED. RAN ENGINE, PER AMM 71-00-00. HPSOV OPERATIONS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT BOOST PUMP) · airframe 88,847 hrs · 25,253 cycles

CENTER LT FUEL PUMP EICAS MESSAGE ON TAXI OUT. FWD TO MDDR 135952, PER MEL 28-22-02A, CAT C, DUE 22OCT20. PLACARD INSTALLED. PERFORMED OPERATIONS CHECK OF LT CENTER BOOST PUMP, PER AMM 28-22-03. OPERATIONS CHECKS OK. THIS CLEARS MDDR 135952, PLACARD REMOVED. DISP LUC @ 01:44Z.

Part: WARNING LIGHT — FALSE INDICATION (CABIN TEMP) · airframe 88,841 hrs · 25,251 cycles

FWD CABIN TRIM LIGHT INOPERABLE IS ON. TRANSFERRED TO MDDR 135921, PER MEL 21-61-06-01-01A, CAT C. DUE 22 OCT 2020. 3 SUCESSFUL LEGS WHEN TEMP CONTROL. OPERATIONS OK, NO FAULTS NOTED. PERFORMED SYSTEM OPERATIONS CHECK, PER AMM 21-61-05. THIS CLEARS MDDR 135921. PLACARD REMOVED. DISP CD AT 2303.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENG ANTI ICE) · airframe 88,814 hrs · 25,245 cycles

RT ENGINE ANTI ICE. OPERATIONS TEST OF RT ENGINE TAI CARRIED OUT, IAW AMM 30-21-03. ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED · airframe 88,805 hrs · 25,243 cycles

AFTER T/O AT APPROX 9000' EICAS MSG "LT ENGINE PRV" DISPLAYED AND WENT AWAY TWICE. NOW "LT ENGINE PRV" STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED LT ENGINE PRV CONTROLLER, IAW AMM REF 36-11-19. OPERATIONS CHECK OK, LEAK CHECK OK. MESSAGE CLEARED. S/N OFF: MTH00887, P/N OFF: 792755-15. REMOVED AND REPLACED AIR SUPPLY BITE MODULE, IAW AMM REF 36-23-01, BITE TEST OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT HPSOV) · airframe 88,726 hrs · 25,225 cycles

LT ENG HPSOV STATUS MSG. LT ENG HPSOV BITE TEST CARRIED OUT, IAW AMM 36-23-00. NO ACTIVE MSG, SELF ERASED.

Part: UNKNOWN — UNKNOWN (APU PNEUMATIC) · airframe 88,720 hrs · 25,223 cycles

APU NO PNEUMATIC OUTPUT. APU RESTARTED, ALL PNEU DUCT PRESSURE NORMAL, IAW AMM 49-11-00. OK FOR SERVICE.

Part: WIRE — LOOSE (SWITCH) · airframe 88,714 hrs · 25,222 cycles

RIGHT ENGINE ANTI ICE VALVE LIGHT INOP. TRANSFERRED TO MDDR 134644, IAW MEL 30-21-02-01A, CAT C. FOUND AND SECURED LOOSE PIN WIRE AT SWITCH, PER AMM 33-13-00. OPS CHECKED NORMAL. THIS CLEARS MDDR 134644. PLACARD REMOVED.

Part: WATER SEPARATOR — CRACKED (LT A/C PACK) · airframe 88,714 hrs · 25,222 cycles

LEFT PACK WATER EXTRACTOR HAS A CRACK AT THE INBOARD TEMP PROBE. REMOVED AND INSTALLED LEFT WATER EXTRACTOR ASSY AND PERFORMED INSTALLATION AND TEST OK, PER AMM 21-51-04.

Part: RELAY — FAILED (ANTI-ICE SYSTEM) · airframe 88,644 hrs · 25,209 cycles

AFTER TURNING OFF RT ENGINE ANTI ICE DURING DESCENT VALVE LIGHT INTERMITTENT BETWEEN OFF/ON. FOUND KORRY SWITCH FAULTY PER FIM 30-21-803. SWITCH ON ORDER, REQUIRES RELAY REPLACEMENT. REPLACED K2 RELAY, IAW WD 30-21-11, SYS OPS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE PRV) · airframe 88,633 hrs · 25,206 cycles

LT ENG PRV MESSAGE, CLEARED MESSAGE PER FIM 36-10-00. PERFORMED ENGINE RUN, PER AMM 71-00-00, NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 88,600 hrs · 25,198 cycles

ON SHORT FINAL, LEFT FWD FUEL PUMP EICAS. FWD FUEL PUMP OPERATIONS CHECK CARRIED OUT IAW AMM 28-22-03. ALL SATISFACTORY AND INDICATE NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PRV) · airframe 88,570 hrs · 25,190 cycles

LT ENG PRV STATUS MESSAGE ON TAXI IN. ENG NR 1 RAN; OPERATIONS CHECK SATISFACTORY IAW AMM 71-00-00. ALL IND NORMAL NO ACTIVE MESSAGES.

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK TEMP) · airframe 88,463 hrs · 25,169 cycles

R PACK TEMP EICAS MSG (PACK TEMPERATURE CONTROL SYSTEMS (-200/-300), AUTO MODE) TRANSFERRED ITEM TO MDDR 133072 PER MEL 21-03-01, CAT C, DUE 28 AUG 20 MCC ALEY DISP SP 2222Z. REMOVED AND REPLACED RH PACK TEMP CONTROLLER BOX REF AMM 21-51-14. OPS CHECKS OK. THIS CLEARS MDDR 133072. NOTIFIED MCC.

Part: PRESSURE SWITCH — FAILED (FWD BOOST PUMP) · airframe 88,442 hrs · 25,164 cycles

FWD BOOST PUMP EICAS MSG ON RECENT HISTORY REMOVED AND REPLACED ;L FWD FUEL PUMP PRESS SWITCH IAW B767 FIM 28-25-00T815. OPS CKS GOOD.

Part: A/C PACK — OVERHEATED (LEFT) · airframe 88,442 hrs · 25,164 cycles

LEFT PACK OVER HEAT ILLUMINATED HISTORY REMOVED, INSPECTED, AND REINSTALLED THE LH PACK OVERHEAT SWITCH REF B767 AMM 21-51-18. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK TEMP) · airframe 88,410 hrs · 25,155 cycles

RIGHT PACK TEMP EICAS DURING CRUISE AT FL 340 1716Z(<P>ACCOMPLISHED FIM 21-51-00-810-877-001. RESET R PACK TEMP CONTROLLER AND OPS CHECKS GOOD PER MM 22-51-00. NO FAULTS.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 88,410 hrs · 25,155 cycles

"L FWD FUEL PUMP" EICAS MSG DISPLAYED. COMPLETED QRH.(<P>ACCOMPLISHED F.M 28-22 TREE 819 AND L FWD BOOST PUMP OPERATES NORMAL AS PER AMM 28-42-01. OK FOR SERVICE, NO FAULTS FOUND.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (PRIORITY VALVE) · airframe 88,353 hrs · 25,143 cycles

LEFT PRV MESSAGE AFTER TAKE OFF. REMOVED AND REPLACED LEFT ENG PRV IAW AMM 36-11-18. LEAK AND OPS CHECK GOOD. NO MESSAGE DISPLAYED.

Part: ACTUATOR — FAILED (SPOILERS) · airframe 88,354 hrs · 25,144 cycles

C HYD SYS PRESS EICAS AND LOSS C HYD FLUID. NUMBER 8 INBD SPOILER PCA FAILED. REMOVED AND REPLACED NUMBER 8 INBD SPOILER PCA RIGHT WING IAW MM 27-61-02. CHECKS GOOD. C HYD SYSTEM SERVICED PER MM 12-12-01.

Part: SHUTOFF VALVE — FAULTED (LT ENGINE) · airframe 88,344 hrs · 25,142 cycles

STATUS MSG L ENG PRV PERFORMED BITE OF AIR SUPPLY SYSTEM IAW AMM 36-23-00. FAULTED L ENGINE HPSOV. REMOVED AND REPLACED L ENG HPSOV IAW 36-11-07. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PACK DUCT) · airframe 88,303 hrs · 25,133 cycles

DUE TO +38 DEGREES C TEMPS OUTSIDE, LT DUCT LEAK LIGHT ON LEFT PACK. NO LEAKS NOTED IAW AMM 21-48-00. OPENED LEFT PACK DOORS TO FACILITATE COOLING, CLOSED PACK BAY DOORS PER AMM 21-51-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 88,256 hrs · 25,119 cycles

LEFT ENG PRV STATUS MSG ENG RUN C/W ON #1 ENG IAW AMM 71-00-00. ALL INDICATIONS NORMAL. NO ACTIVE MSG. OK FOR SERVICE. OPS CHECK OF PRV IAW AMM 36-11-07. OPS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 88,180 hrs · 25,104 cycles

ON APPROACH EICAS MESSAGE FOR LT FWD FUEL PUMP. PERFORMED CIRCUIT BREAKER RESET IAW AMM 28-25-00, TEST OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 88,198 hrs · 25,108 cycles

LEFT ENGINE PRV STATUS MESSAGE. PERFORMED AIR SUPPLY MODULE BITE TEST IAW AMM 36-00-30, NO FAULTS.

Part: UNKNOWN — UNKNOWN (APU) · airframe 88,173 hrs · 25,102 cycles

NO APU AIR PRESSURE AFTER ENG SHUTDOWN. SHUTDOWN APU AND RESTARTED IAW AMM 49-11-00. OPS CHECKED GOOD.

Part: TRANSDUCER — MALFUNCTIONED (APU AIR DUCT) · airframe 88,144 hrs · 25,096 cycles

APU AIR RIGHT DUCT PRESSURE INDICATING 0 ON DUCT PRESSURE GAUGE AND ECS. REMOVED AND REPLACED THE RT BLEED PRESSURE TRANSDUCER IAW AMM 36-21-01, OPS CHECK GOOD.

Part: GENERATOR — TRIPPED (APU) · airframe 88,144 hrs · 25,096 cycles

APU GENERATOR OFF EICAS MESSAGE AFTER APU START ON LANDING. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECKED GOOD.

Part: ELT — DAMAGED (CABIN) · airframe 88,142 hrs · 25,095 cycles

MAIN DECK FWD CLOSET ELT DAMAGED. REMOVED AND REPLACED ELT AT FWD CLOSET PER AMM 25-63-00.

Part: CARTRIDGE — BROKEN (L1 DOOR) · airframe 88,142 hrs · 25,095 cycles

L1 DOOR POPS WHEN OPEN. FOUND L1 DOOR FWD CARTRIDGE LIMITING OVERHEAD DOOR BROKEN. REMOVED AND REPLACED CARTRIDGE. AMM 52-11-21 AND COUNTER BALANCE SYSTEM AMM 52-11-16 OPS TEST AND CHECK OK.

Part: ELT — DAMAGED (LT CABIN) · airframe 88,142 hrs · 25,095 cycles

MAIN DECK LH AFT STORAGE COMPARTMENT ELT DAMAGED. REMOVED AND REPLACED ELT AT AFT STORAGE COMPARTMENT. AMM 25-63-00.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 88,142 hrs · 25,095 cycles

LEFT SIDE, ONE EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-00, OPS CHECKED OK.

Part: DUCT — LEAKING (LT A/C PACK) · airframe 88,144 hrs · 25,096 cycles

LT PACK DUCT P/N 2202317-1 HAS LEAK AT TEMP PROBE. REMOVED &AMP; REPLACED LT PACK DUCT AS PER AMM 20-11-00. LEAK CHECK PERFORMED, NO LEAKS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 88,101 hrs · 25,086 cycles

FWD EQUIPMENT OVERHEAT EICAS MESSGAE ILLUMINATED AFTER DEPARTURE. IAW QRH SELECTED EQUIPMENT COOLING SWITCH TO STANDBY THEN OVRD, CLEARING THE PROBLEM. OAT WAS 117ºF, EXTENDED GROUND TIME, TAXI AND HOLD FOR TAKE OFF. OAT STILL AT 10C AT 30K FT. AFTER REACHING COOL. SPS OPS NORMAL, C/W FIM 21-58 F/T 910. OAT ABOVE 110C WITH NO DEFECTS NOTED. SYSTEM OPS CHECKED AND BITE CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,101 hrs · 25,086 cycles

STATUS MSG CABIN ALT AUTO 2 ILLUMINATED. C/W FIM 21-31 F/T 803. NO FAULTS FOUND. CABIN ALT 2 OPS CKS GOOD AT THIS TIME.

Part: SWITCH — UNSECURE (FUEL SYSTEM) · airframe 88,090 hrs · 25,083 cycles

LT FWD FUEL PUMP EICAS BLED PRESSURE SWITCH SENSE LINE FOR LT BOOST PUMP, RE-SECURED SWITCH AND LINE. LT FWD BOOST PUMP AND PRESS LIGHTS OPS CK NORMAL IAW AMM 28-42-01.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 88,101 hrs · 25,086 cycles

CABIN ALT AUTO 2, REMOVED AND REPLACED NR 2 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. OPS CHK GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 88,101 hrs · 25,086 cycles

LEFT PACK TEMP MSG ON ECS PLUS PREVIOUS HISTORY. REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHK GOOD.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 87,999 hrs · 25,062 cycles

LEFT ENG TAI VALVE EICAS MESSAGE. REMOVED AND REPLACED TAI VALVE ON LEFT ENGINE IAW AMM 30-21-03. OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 87,990 hrs · 25,060 cycles

L FWD FUEL PUMP EICAS MESSAGE. PERFORMED OPS CHECK PER AMM 28-22-00. OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 88,017 hrs · 25,066 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED CABIN PRESSURE CONTROLLER BITE PROCEDURE IAW FIM 21-31-00/101, NO FAULTS NOTED. MESSAGE CLEARED. OPS OK.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 87,929 hrs · 25,047 cycles

LEFT A/C PACK TEMP EICAS IN FLIGHT. PERFORMED FIM 21-51 TASK / 877. LEFT PACK CONTROLLER BITES SHOWS TEMP VALVE FAULT. PERFORMED A RESET OF THE LEFT PACK CONTROLLER. NO FAULTS DISPLAYED. OPS TESTED GOOD IAW AMM 21-51-00.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 87,907 hrs · 25,042 cycles

CAB ALT 2 AUTO EICAS MSG. RESET CABIN PRESSURE / CONTROLLER, IAW AMM 21-31-02. SYS TEST, SAT IS NO FAULTS ACTIVE, DMI 130049 / CLEARED, MCC INFORMED.

Part: MOTOR — FAULTED (CABIN PRESSURE) · airframe 87,813 hrs · 25,021 cycles

CABIN ALTITUDE 2 STATUS MESSAGE. PERFORMED BITE IAW FIM 21-31-00, FAULTED AC MOTOR, RESET FAULTS. PERFORMED ANOTHER BITE. NO FAULTS NOTED. AC OK FOR SERVICE.

Part: MOTOR — FAILED (CABIN PRESSURE) · airframe 87,800 hrs · 25,018 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. BITE ON CONTROLLER FAULTS A/C MOTOR. REMOVED AND REPLACED THE CABIN ALTITUDE NR 2 AC MOTOR IAW AMM 21-31-05, OPS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,779 hrs · 25,015 cycles

LT FWD FUEL PUMP EICAS MESSAGE ON TAXI-IN. LT FWD FUEL PUMP WORKING IAW AMM 28-42-00, ALL SATISFACTORY.

Part: DUCT — DAMAGED (APU BAY) · airframe 87,794 hrs · 25,017 cycles

APU AIR SURGES WHILE TRYING TO OPERATE BOTH PACKS ON THE GROUND. VISUAL INSPECTION CARRIED OUT IN APU COMPARTMENT AREA. HOLE FOUND IN DUCT CONNECTED TO SURGE CONTROL VALVE. OLD BROKEN DUCT REMOVED AND NEW ONE FITTED. OPS CHECK GOOD. REF AMM 49-53-01-004-001.

Part: CONTROL VALVE — INOPERATIVE (RT A/C PACK) · airframe 87,767 hrs · 25,012 cycles

RT PACK INOPERATIVE. REMOVED AND REPLACED THE RT FLOW CONTROL VALVE ASSY IAW AMM 21-51-01, OPS CHECK OF RIGHT PACK WAS GOOD.

Part: FIRE LOOP — FAILED (LT ENGINE) · airframe 87,767 hrs · 25,012 cycles

L ENG FIRE LOOP 2 MESSAGE WILL NOT RESET. FOUND UPPER AFT AND LOWER AFT LOOPS NR 2 BAD. REMOVED AND REPLACED THE NR 1 ENGINE AFT LOWER FIRE DETECTOR IAW AMM 26-11-02. OPS CHECKED GOOD. FAULTING UPPER AFT DETECTOR. REMOVED AND REPLACED AFT UPPER FIRE LOOP NR 1 IAW AMM: 26-11-02. OPS CHECK PERFORMED, NO FAULTS FOUND.

Part: PLUG — DAMAGED (APU) · airframe 87,733 hrs · 25,005 cycles

APU DRAIN PLUG FOUND DAMAGED. REMOVED DRAIN PLUG FROM APU AND INSTALLED ON NEW APU. OPERATIONAL AND LEAK CHECK OK IAW AMM 49-27-01, MCC NOTIFIED.

Part: CLAMP — LEAKING (APU) · airframe 87,733 hrs · 25,005 cycles

V BAND CLAMP LEAKING ON DUCT ON APU. REMOVED AND REPLACED V BAND CLAMP. OPERATIONAL CHECK NORMAL. LEAK CHECK NORMAL IAW AMM 49-11-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

SCRIBE LINE DAMAGES WERE FOUND AROUND ADF ANTENNA NR 1, BETWEEN STA 1109 / STA 1131 AND ADF ANTENNA NR 2, BETWEEN STA 1153 / STA 1175. BOTH OF THEM ON THE CROWN AREA BETWEEN STRINGERS S-1L AND S-1R.DAMAGES WERE REPAIRED IN ACCORDANCE WITH MRO TRE6753358 R1.

Part: O2 GENERATOR — INOPERATIVE (LAVATORY) · airframe 87,702 hrs · 24,998 cycles

FWD CABIN AFT LAVATORY INOP TRANSFERRED TO DMI 128701 IAW MEL 38-30-01B, CAT 'C'. REMOVED AND REPLACED FWD CABIN AFT LAV LT SIDE O2 GENERATOR PER AMM 35-21-13. NO FURTHER DEFECTS NOTED. MMC NOTIFIED. PLACARDS REMOVED. THIS CLEARS DMI 128701.

Part: SKIN — GOUGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

GOUGE ON FUSELAGE SKIN CROWN AREA, BETWEEN STA 236.50 AND STRINGER S-2R. REPAIRED IN ACCORDANCE WITH MRO TRE6753356.

Part: SKIN — GOUGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

SCRATCH AND GOUGE ON FUSELAGE SKIN BETWEEN STA 764 AND S-1L / S-1R. DAMAGES REPAIRED IN / ACCORDANCE WITH TRE6753353.

Part: LIFE RAFT — UNSERVICEABLE (CABIN) · airframe 87,700 hrs · 24,997 cycles

DURING MAINTENANCE VISIT AT MRO, THE CABIN PAX LIFE RAFT WAS FOUND WITH COVER DISJOINTED P/N R0202A211. THE PART WAS REQUESTED FOR / REPLACEMENT, HOWEVER THE LEAD TIME OF THE PART IS OUT OF THE AIRCRAFT RETURN TO / SERVICE DUE DATE AND THE NRC IS DEFERRED IAW MEL;25-62-01, MDDR 128702, CAT 'D'. REMOVED AND REPLACED CABIN PAX LIFE RAFT IAW AMM 25-62-00. THIS CLEARS DMI 128702, MCC NOTIFIED AMM 1600Z.

Part: SKIN — GOUGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

DENT + GOUGE ON FUSELAGE SKIN BETWEEN STA 390 / STA 412 AND STRINGERS S-22L / S-23L. DAMAGES REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-1 REPAIR 1.

Part: SKIN — GOUGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

GOUGE DAMAGE ON FUSELAGE SKIN BETWEEN STA 982 AND STRINGER S-3L. REPAIRED IN ACCORDANCE WITH MRO TRE6753355.

Part: SKIN — BULGED (FUSELAGE) · airframe 87,700 hrs · 24,997 cycles

BULGE DAMAGE ON THE FUSELAGE SKIN BETWEEN STA 1654.50 / STA 1725.50 AND STRINGER S-32L / S-34L. DAMAGE REPAIRED PER SRM 53-00-01-2R-29 REPAIR 29.

Part: APU — FAILED · airframe 87,702 hrs · 24,998 cycles

APU FAILED TO START SEVERAL TIMES. REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECK GOOD.

Part: TRANSMITTER — MALFUNCTIONED (APU OIL SYSTEM) · airframe 87,673 hrs · 24,991 cycles

APU OIL QUANTITY INOP, FLUCTUATES FROM ADD TO FULL AND ALL POINTS IN BETWEEN. VERIFIED OIL QTY IS FULL BY VISUAL SIGHT GLASS. APU OIL QTY TRANSMITTER WAS REPLACED IAW AMM 49-94-04-404-004.

Part: TRANSMITTER — FAULTY (APU) · airframe 87,664 hrs · 24,990 cycles

APU OIL QUANTITY INDICATOR FLUCTUATES IN FLIGHT.(<P>REMOVED AND REPLACED OIL QUANTITY TRANSMITTER IAW AMM 49-94-04, OPS CHECKS GOOD.</P>)

Part: PUMP — DEFECTIVE (FUEL SYSTEM) · airframe 87,664 hrs · 24,990 cycles

L/H CTR OVERRIDE PUMP DOESN'T PUT OUT ENOUGH PRESSURE.(<P>REMOVED AND REPLACED L/H CTR OVERRIDE PUMP, REF 28-22-05. OPS AND LEAK CHECK OK.</P>)

Part: FUEL LINE — OBSTRUCTED (FUEL SYSTEM) · airframe 87,644 hrs · 24,988 cycles

L FWD FUEL PUMP CAUTION MSG APPEARED AFTER LANDING (INTERMITTENT).(<P>REMOVED PRESSURE SWITCH, PURGED, CLEAN AND INSPECTED FUEL PRESSURE LINE. REINSTALLED PRESSURE SWITCH AND CLEAN CONNECTOR IAW AMM 28-42-01. OPS CHECK GOOD. LEAK CHECK GOOD.</P>)

Part: MEDICAL KIT — MISSING (CABIN) · airframe 87,582 hrs · 24,976 cycles

FORWARD CABIN EMERGENCY MEDICAL KIT MISSING.(<P>INSTALLED&NBSP;MISSING FORWARD CABIN MEDICAL KIT IAW WORK CARD NUMBER A-25-099-20-01.</P>)

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 87,521 hrs · 24,963 cycles

LT FWD FUEL PUMP PRESS EICAS ON FINAL APPROACH.(<P>LH FWD FUEL PUMP PRESSURE SWITCH CONNECTOR CLEANED AND RESET I.A.W AMM 28-42-01. OPS CHECK SATISFACTORY, ALL INDICATIONS NORMAL.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,482 hrs · 24,955 cycles

L FWD FUEL PUMP EICAS, QRH COMPLETE.(<P>L FWD PUMP OPS CHECK NORMAL PER FIM 28-22 TREE 819.</P>)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 87,414 hrs · 24,943 cycles

LEFT SIDE WINDOW HEAT SWITCH WILL NOT STAY IN.(<P>REMOVED AND REPLACED WINDOW HEAT PANEL ASSY IAW B767 AMM 30-41-02. OPS CHECK NORMAL.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 87,414 hrs · 24,943 cycles

LEFT FWD FUEL PUMP CAUTION.(<P>REMOVED AND REPLACED LEFT FWD PRESSURE SWITCH (LEFT FUEL PRESSURE). OPS CHECKED NORMAL IAW B767 AMM 28-42-01.&NBSP;</P>)

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 87,365 hrs · 24,937 cycles

LEFT FUEL PUMP PRESS LIGHT ILLUMINATED W/ EICAS ON LANDING.(<P>CLEANED C/P ON LT FWD BOOST PUMP PRESSURE SW, OPS CHK NORMAL PER AMM 28-42-02.</P>)

Part: RELAY — FAILED (BOOST PUMP) · airframe 87,299 hrs · 24,926 cycles

L FWD FUEL PUMP EICAS MESSAGE DISPLAYED AFTER TOUCHDOWN.(<P>ITEM TRANSFERRED TO MDDR 125004 PER MEL 28-22-01. ITEM IS CAT C, DUE 04MAR20. MX ACTION C/W. ALL PLACARDS INSTALLED. MCC NOTIFIED.</P><P>LP 1048618 - ITEM M3: AS PER WD 28-22-11, REPLACED K10703 GFI RELAY. OPS TESTED LEFT FWD BOOST PUMP IAW AMM 28-22-00, TESTED OK. THIS CLEARS MDDR 125004. PLACARD REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 87,289 hrs · 24,924 cycles

APU FAULT EICAS MSG.(<P>A/C IS IN MAINTENANCE.</P><P>INSPECTED APU FOR FAULTS, APU CONTROLLER SHOWED NO FAULTS, NO MESSAGE ON EICAS, OPERATED APU THRU SEVERAL CYCLES, NO FAULTS NOTED PER AMM 49-11-00.</P>)

Part: PRESSURE SWITCH — WARNING MESSAGE (LT FUEL PUMP) · airframe 87,260 hrs · 24,920 cycles

L FWD FUEL PUMP EICAS MESSAGE.(<P>TRANSFERRED TO MDDR #124856 IAW MEL 28-22-01, CAT C, DUE 29FEB20. PLACARD INSTALLED. MCC NOTIFIED AND MX PROCEDURE C/W.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 87,250 hrs · 24,919 cycles

DURING APPROACH LH FWD FUEL PUMP MESSAGE APPEARED. RAN QRH.(<P>NO EICAS MSG PRESENT. ACCOMPLISHED OPS CHECK FOR THE LH FWD FUEL PUMP PER AMM 28-22-00. OPS CHECK GOOD. MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 87,220 hrs · 24,911 cycles

L FWD FUEL PUMP.(<P>OPS CHECKED L/H FWD FUEL BOOST PUMP IAW B767 AMM 28-22-00, OPS CHECK GOOD. NO EICAS MESSAGES DISPLAYED.</P>)

Part: PUMP — FAILED (FUEL BOOST) · airframe 87,163 hrs · 24,899 cycles

L FWD FUEL PUMP EICAS MSG ON LANDING.(<P>TRANSFERRED TO MDDR 124422 PER MEL 28-22-01, CAT 'C', DUE 18FEB20.</P><P>REF LOG PAGE 1226141: REMOVED AND REPLACED L/H FWD BOOST PUMP PER AMM 28-22-03. OPS AND LEAK CHECKS GOOD. THIS CLEARS MDDR 124422. PLACARD REMOVED.</P>)

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 87,197 hrs · 24,906 cycles

CA SIDE SMOKE GOGGLES HEADSTRAP NEEDS REPLACEMENT. STRAP IS LOOSE AT TIGHTEST ADJUSTMENT. STRAP LOOSENS ON ITS OWN FROM TIGHTEST ADJUSTMENT.(<P>REMOVED AND REPLACED&NBSP;CA SIDE SMOKE GOGGLES IAW B67 AMM 25-64-00.<BR /></P>)

Part: ACTUATOR — FAILED (RAM AIR INLET) · airframe 87,160 hrs · 24,898 cycles

R PACK TEMP EICAS IN FLIGHT FL 390 LEVEL FLIGHT. QRH COMPLIED WITH. R PACK CONTROL SELECTOR REMAINS AT STBY N.(<P>REMOVED AND REPLACED RH RAM AIR INLET DOOR ACTUATOR IAW B767 AMM 21-53-03. BITE RH TEMP CONTROLLER TEST GOOD. REFER TO ITEM M19 LP 1226188 FOR OPERATIONAL CHECK OF THE PACK OUTLET TEMP CONTROLLER IAW B767 AMM 21-51-14.</P><P>LP 1226188 - ITEM M19: PERFORMED OPS CHECK OF THE R PACK IAW B767 AMM 21-53-03, OPS CHECK GOOD AT THIS TIME.</P>)

Part: ISOLATION VALVE — STICKING (LEFT) · airframe 87,127 hrs · 24,893 cycles

L ISLN VALVE STICKING AND SLOW TO OPEN.(<P>L ISLN VALVE REMOVED AND REPLACED IAW AMM 36-11-04. OPS CHECK SATISFACTORY, ALL INDICATIONS NORMAL.</P>)

Part: OXYGEN MASK — INOPERATIVE (FIRST OFFICER'S) · airframe 87,124 hrs · 24,892 cycles

F/O O2 MASK HARNESS INOP.(<P><SPAN>O2 MASK REMOVED FROM 2ND OBS POSITION AND USED AT F/O POSITION.</SPAN><SPAN>&NBSP;</SPAN>OPS CHK SATISFACTORY, NO LEAKS NOTED. NOW 2ND OBS O2 MASK INOP.</P><P>LP 1226171 - ITEM 5: 2ND OBS O2 MASK INOP TRANSFERRED TO DMI 124232 IAW DDG 25-11-02-02, CAT 'D'.</P><P>LP&NBSP;1226172 - ITEM 3: REMOVED AND REPLACED 2ND OBS O2 MASK. LEAK AND OPS CHECKED OK PER AMM 35-11-51. THIS CLEARS MDDR 124232. PLACARD REMOVED.</P>)

Part: STATUS MESSAGE — ILLUMINATED (LT FUEL FILTER) · airframe 87,069 hrs · 24,882 cycles

L ENG FUEL FILTER STATUS MSG.(<P>REMOVED AND REPLACED L ENG FUEL FILTER IAW AMM 73-11-02, NO LEAKS NOTED.</P>)

Part: GARLOCK SEAL — LEAKING (IDG) · airframe 86,996 hrs · 24,870 cycles

NR 1 ENGINE HAS HIGH OIL CONSUMPTION. FOUND IDG GARLOCK SEAL LEAKING. DRAIN LINE CAPPED IAW AMM 71-71-00. REMOVED LEFT IDG, REMOVED AND REPLACED LH IDG DRIVE CARBON SEAL IAW AMM 72-64-02. INSTALLED LT IDG IAW AMM 24-11-01. RUN AND LEAK CHECKED OK IAW AMM 71-00-00. DRAIN LINE RESTORED.

Part: WIRE — DAMAGED (RELAY K1231) · airframe 86,988 hrs · 24,869 cycles

RIGHT ENGINE IGNITOR 1 WAS INOPERATIVE. REMOVED AND REPLACED THE IGNITER PLUG NR 1 IAW AMM 74-21-02, NO HELP. REMOVED AND REPLACED RH ENGINE IGNITION EXCITER IAW AMM 74-11-01, NO HELP. FOUND BAD WIRE ON P37 AT RELAY K1231 (WDM 74-31-21). REPAIRED WIRE IAW SWPM 20-81-12. RT ENGINE IGNITION 1 & 2 TESTED GOOD IAW AMM 74-00-00. DMI 123685 CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E EXHAUST FAN) · airframe 86,966 hrs · 24,865 cycles

AFT EQ EXH FAN 1 STATUS MESSAGE. PERFORMED FIM TASK 21-26 FT 805. SYSTEM OK, MESSAGE CLEARED.

Part: GENERATOR — INOPERATIVE (APU) · airframe 86,940 hrs · 24,860 cycles

APU GENERATOR INOPERATIVE. PERFORMED A BITE ON BPCU, FAULTS GENERATOR DIODE. REMOVED AND REPLACED THE APU GENERATOR IAW AMM 24-21-01. OPS CHECKED GOOD, LEAK CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,929 hrs · 24,857 cycles

EICAS "LH FWD FUEL PUMP"(<P>PERFORMED OPERATIONAL CHECK PER AMM 28-22-00. NO FAULTS NOTED. SYSTEM OK FOR SERVICE.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 86,912 hrs · 24,853 cycles

L PACK TEMP EICAS, PERFORMED BITE ON LT PACK CONTROLLER IAW FIM 21-51-00. FAULT LT PACK TEMP CONTROL VALVE. REMOVED AND REPLACED THE TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECKED NORMAL,

Part: ACTUATOR — FAILED (LT RAM AIR DOOR) · airframe 86,878 hrs · 24,846 cycles

LEFT PACK INOPERATIVE IN AUTO. OPS CHECKED OK IN STBY. REMOVED AND REPLACED LEFT RAM DOOR ACTUATOR IAW AMM 21-53-02. OPS CHECK OK .

Part: CONNECTOR — DISCONNECTED (PRESSURE SWITCH) · airframe 86,878 hrs · 24,846 cycles

LEFT ENGINE FWD FUEL PUMP LOW PRESS LIGHT WILL NOT SHUT OFF. CONFIRMED LH FWD FUEL PUMP OPERATING OK. LOW PRESSURE LIGHT DOES NOT TURNOFF. FOUND THE CONNECTOR TO THE LEFT FWD PRESSURE SWITCH NOT INSTALLED ON SWITCH. CONNECTED THE CONNECTOR TO THE SWITCH. LEFT FWD PRESSURE SWITCH CHECKED OK IAW AMM 28-42-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,872 hrs · 24,845 cycles

LEFT PACK TEMP EICAS, RAN THE QRH/NNL AND REMAINED IN STBY.(<P>PREFORMED BITE ON PACK TEMP CONTROLLER, FAULT FOR RAM ACTUATOR - CLEARED FAULTS, RAN BITE AGAIN. NO MX FAULTS. SYS OK FOR SERVICE PER FIM 21-51-00.</P>)

Part: PUMP — FAILED (LT FUEL BOOST) · airframe 86,820 hrs · 24,830 cycles

L FWD FUEL PUMP EICAS MESSAGE ON DESCENT. TROUBLESHOOTING PERFORMED FIM 28-22 FAULT TREE 819 TO STEP 50, BLED THE PRESSURE SENSE LINE. INSPECTED SENSE LINE IAW FIM 28-22 FT 819. NO WATER OR DEBRIS FOUND. REMOVED AND REPLACED THE LT FWD FUEL PUMP IAW AMM 28-22-03. OPS AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 86,811 hrs · 24,828 cycles

LEFT PACK TEMP EICAS MESSAGE, PER QRH PACK SELECTOR TO STBY N, MESSAGE WENT OUT. PERFORMED OPS TEST IAW AMM 21-51-00. OPS CHECKED GOOD.

Part: PSEU — FAILED (FWD E/E VALVE) · airframe 86,808 hrs · 24,826 cycles

FWD EQPT VALVE EICAS MESSAGE. REMOVED AND REPLACED PSEU IAW AMM 32-09-04. OPS CHECKED GOOD. PERFORMED AUTO SPEED BRAKE SYS TEST AND OPS TEST IAW AMM 27-62-00. OPS CHECKED GOOD.PERFORMED OPS TEST IAW AMM 21-23-08, OPS TESTED GOOD.

Part: ACTUATOR — FAILED (SPAR VALVE) · airframe 86,804 hrs · 24,825 cycles

DURING START LEFT ENGINE SPAR VALVE LIGHT DID NOT ILLUMINATE. ENGINE STABILIZED AND SHUT DOWN BY ITSELF. REMOVED AND REPLACED LEFT SPAR VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED GOOD.

Part: ISOLATION VALVE — FAILED (LEFT) · airframe 86,804 hrs · 24,825 cycles

LEFT BLEED ISOLATION VALVE EICAS MESSAGE.(<P>REMOVED AND REPLACED LEFT BLEED ISOLATION VALVE IAW AMM 36-11-05-404-013. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK TEMP) · airframe 86,786 hrs · 24,822 cycles

L PACK TEMP EICAS CAUTION, PERFORMED QRH 2.51. MESSAGE EXTINGUISHED. PERFORMED AN OPS TEST IAW AMM 21-51-00, OPS CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (ALTIMETER) · airframe 86,791 hrs · 24,823 cycles

CAPTAIN'S RADAR ALT PROVIDING/DISPLAYING ERRONEOUS INDICATIONS ON DESCENT BELOW 8000.&NBSP;(<P>PERFORMED OPS TEST IAW AMM 34-43-00. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ISOLATION VALVE) · airframe 86,770 hrs · 24,817 cycles

L ISLN VALVE EICAS BLEED.(<P>PERFORMED GROUND TEST I.A.W AMM 36-11-04. OPS CHECK GOOD.</P>)

Part: CAP — LOOSE (DRAIN LINE) · airframe 86,767 hrs · 24,816 cycles

FUEL LEAKING FROM LEFT ENGINE.(<P>UPON INSPECTION FOUND FUEL TRANSMITTER DRAIN LINE CAP LOOSE. TIGHTENED I.A.W AMM 70-50-00. WET MOTORED ENGINE FOR LEAK CHECK I.A.W AMM 71-00-00. NO LEAKS. OPS CHECK GOOD.&NBSP;</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,746 hrs · 24,807 cycles

EMERGENCY LIGHTS AT RIGHT AISLE CEILING INOP (ROW 22JL).(<P>REMOVED AND REPLACED BATTERY PACK ASSY IAW B767 AMM 33-51-07, OPS CHECK OK.</P>)

Part: FILTER — WARNING MESSAGE (RT ENG FUEL) · airframe 86,745 hrs · 24,806 cycles

RIGHT ENGINE FUEL FILTER STATUS/EICAS MESSAGE.&NBSP;(<P>REMOVED AND REPLACED RIGHT ENGINE FILTER REF AMM 73-11-02-004-001-H00, NO LEAKS NOTED. PERFORMED FUEL FILTER INSPECTION, NO DAMAGE FOUND IN REF 73-11-03-202-001-H00. PERFORMED ENGINE RUN, NO MESSAGES, ALL NORMAL REF AMM 71-00-00.</P>)

Part: VALVE — FAILED (E/E COOLING) · airframe 86,741 hrs · 24,805 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE. REMOVED AND REPLACED EQUIPMENT COOLING INDICATION CARD IAW AMM 21-58-24, NO HELP. REMOVED AND REPLACED THE MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01. OPERATIONAL CHECKS PERFORMED IAW AMM 21-58-01-005. CHECKED GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE BLEED) · airframe 86,741 hrs · 24,805 cycles

AFTER ENG START, "RH ENG BLEED" MSG. NO DUCT PRESSURE.&NBSP;(<P>PER CUSTOMER REQUEST, REMOVED AND REPLACED R/H PRSOV IAW B767 AMM 36-11-09, OPS CHECK REQUIRED.</P><P>LP 1112969 - ITEM M22: PERFORMED OPERATIONAL CHECK OF&NBSP;R/H PRSOV IAW AMM 36-11-09, NO FAULTS OR DEFECTS NOTED.&NBSP;</P>)

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (RT ENGINE) · airframe 86,727 hrs · 24,801 cycles

RT ENGINE BLEED FAILED TO PRESSURIZE.(<P>PERFORMED AIR CONTROL MODULE BITE TEST, MSG PRSOV ON RIGHT ENG. AFTER BITE, RESET, AND PERFORMED ENG RUN. OPS CHECK OK IN REF AMM 36-23-00 AND AMM 71-00-00.</P>)

Part: WIRE — DAMAGED (OIL PRESSURE) · airframe 86,688 hrs · 24,793 cycles

LEFT ENGINE OIL PRESSURE NOT SHOWING ON EICAS.(<P>TEMPORARILY REPAIRED WIRE W5322-301R-18 IAW SWPM 20-10-13. LEFT ENGINE OIL PRESSURE INDICATION OPS CHK GOOD IAW AMM 79-32-00.<BR /></P>)

Part: CONNECTOR — DIRTY (FUEL PUMP) · airframe 86,640 hrs · 24,779 cycles

LEFT FWD FUEL PUMP DISPLAYED EICAS ON FINAL APPROACH, WENT AWAY SHORT FINAL.(<P>CLEANED CONNECTOR FOR THE LEFT FORWARD FUEL PUMP PRESSURE SWITCH. PUMP OPS CHECK GOOD IAW AMM 28-22-03.</P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 86,635 hrs · 24,778 cycles

L FWD FUEL PUMP INOP AFTER LANDING.(<P>PERFORMED OPS CHECK OF THE LEFT FORWARD FUEL PUMP IAW AMM 28-22-03, OPS CHECK GOOD AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 86,600 hrs · 24,772 cycles

EICAS MESSAGE FOR LT FWD FUEL PUMP. CYCLED LT FWD FUEL PUMP CIRCUIT BREAKER IAW AMM 28-22-01, OPS CHECKED OK. MESSAGE CLEARED IAW AMM 28-22-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 86,537 hrs · 24,758 cycles

ON APPROACH, LEFT FORWARD FUEL PUMP EICAS MESSAGE.&NBSP;(<P>PERFORMED OPS TEST IAW AMM 28-22-00, OPS CHECK GOOD.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 86,499 hrs · 24,751 cycles

L FWD FUEL PUMP PRESS, QRH COMPLETED.(<P>PERFORMED OPS TEST IAW AMM 28-22-00, OPS CHECK GOOD.</P>)

Part: SENSOR — MALFUNCTIONED (FAN AIR TEMP) · airframe 86,499 hrs · 24,751 cycles

"LEFT ENGINE HPSOV" EICAS MSG, QRH COMPLETED.(<P>TRANSFERRED TO MDDR #119459 IAW MEL 36-11-02-02, CAT C, DUE: 31-OCT-19. MCC NOTIFIED AND PLACARD INSTALLED.&NBSP;</P><P>LP 1112974 - M10: REMOVED AND REPLACED FAN AIR TEMP SENSOR PER B767 AMM 36-11-17. PERFORMED TUMB CHECK OF THE HPSOV AND CONTINUITY CHECK OF SWITCHES PER WDM 36-11-61. LEAK AND OPS CHECK FOUND NORMAL PER AMM 36-11-17 AND AMM 71-00-00. THIS CLEARS MDDR 119459. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,480 hrs · 24,748 cycles

L ENG HPSOV EICAS MESSAGE, QRH COMPLETED.&NBSP;(<P>TRANSFERRED TO MDDR #119359 IAW AMM 36-11-02-02, CAT C, DUE DATE: 29-OCT-19. MCC NOTIFIED AND PLACARD INSTALLED.</P><P>LP 1210888 - M4: REMOVED AND REPLACED L/H BLEED AIR CONTROL CARD IAW AMM TASK 36-11-12-404-026. RAN ENGINE IAW AMM 71-00-00, OPS CHECK NORMAL. THIS CLEARS MDDR #119359. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 1JL) · airframe 86,470 hrs · 24,745 cycles

DURING LANDING, THE ONBOARD MX REP REPORTED AN O2 MASK DEPLOYED. REPACKED MASK @ 1 JL IAW AMM 35-21-14, OPS CHECK GOOD.</P>)

Part: SHUTOFF VALVE — NOT REPORTED (LEFT ENGINE) · airframe 86,472 hrs · 24,746 cycles

IN-FLIGHT L ENG HPSOV. CHECKLIST COMPLETED, 3RD WRITE UP.&NBSP;(<P>REMOVED AND REPLACED HPSOV PER AMM 36-11-07. LEAK CHECKS OK AND OPS CHECKS NORMAL.</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,459 hrs · 24,741 cycles

L ENG HPSOV EICAS. ALL MAINTENANCE PROCEDURES COMPLIED WITH. REMOVED AND REPLACED HIGH PRESSURE CONTROLLER IAW AMM 36-11-08, OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 86,450 hrs · 24,740 cycles

LEFT ENG HPSOV EICAS MESSAGE DISPLAYED AND ASSOCIATED STATUS MESSAGE. ACCOMPLISHED QRH CHECKLIST. PERFORMED AIR SUPPLY CONTROL SYSTEM BITE IAW AMM 36-23-00, STATUS CLEARED. COMPLIED WITH HPSOV TEST IAW AMM 36-11-07, NO DEFECTS FOUND AT THIS TIME.

Part: IGNITER — FAILED (RT ENGINE) · airframe 86,399 hrs · 24,729 cycles

RIGHT ENGINE DID NOT LIGHT OFF ON FIRST ATTEMPT, SECOND ATTEMPT SUCCESSFUL. STATUS MSG R ENG IGNITER 1. REMOVED AND REPLACED RIGHT ENGINE IGNITER NR 1 PER AMM 74-21-02. PERFORMED RIGHT ENGINE AUDIBLE CHECK PER AMM 74-00-00-730-803-H03. OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG IGNITION) · airframe 86,366 hrs · 24,724 cycles

RT ENG IGNITION STATUS MESSAGE. RH ENG NO IGNITION WITH SINGLE IGN SELECTED ON FIRST START ATTEMPT. START SUCCESSFUL IN BOTH. PERFORMED RT ENGINE START AT THE GATE. ALL INDICATIONS NORMAL IN SINGLE SOURCE IGNITION START IAW AMM 71-00-00.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,268 hrs · 24,704 cycles

EICAS RT ENG BLEED OFF. REF DMI # 118236, RT ENGINE HPSOV LOCKED CLOSED PER 36-11-02-02. DISP: YK @ 13:13Z. LP1210839 - M2: REMOVED AND REPLACED RIGHT ENGINE HPSOV. OPS CHECK AND ALL INDICATIONS NORMAL. ENGINE RUN PER AMM 71-00-00 AND 36-11-07. OFF PART (PN: 790270-14, SN: 880311) LP 1210839 - M3: REMOVED AND REPLACED RIGHT ENGINE HP CONTROLLER PER AMM 36-11-08. OPS AND INDICATIONS NORMAL. ENGINE RUN IAW AMM 71-00-00. THIS CLOSED MDDR 118236.

Part: CONTROL SWITCH — MALFUNCTIONED (AC PACK) · airframe 86,219 hrs · 24,697 cycles

HI FLOW INHIBIT MESSAGE. PERFORMED FIM 21-51 FAULT TREE 813. CYCLED LT & RT PACK CONTROL SWITCHES, SYSTEM OPERATIONAL CHECK SATISFACTORY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,219 hrs · 24,697 cycles

LT ENGINE VALVE LIGHT CAME ON. PERFORMED ENGINE RUNS IAW AMM 71-00-00, TEST 3. OPERATIONAL TEST NORMAL. AIRCRAFT RELEASED TO CONTINUE ETOPS SERVICE.

Part: WIRE HARNESS — UNSECURE (ENGINE) · airframe 86,191 hrs · 24,693 cycles

4.3 UNITS FAN VIBRATION ON LEFT ENGINE INDICATED ON CLIMB OUT. ACCOMPLISHED FIM 71-05 FT 853. SECURED WIRING HARNESS IAW AMM 70-24-05. SECURED HOLD OPEN ROD IAW AMM 71-11-00. NO ISSUES NOTED ON ENGINE RUN, VIBE AT 1.8 UNITS.

Part: WIRE — BROKEN (WINDOW HEAT) · airframe 86,145 hrs · 24,685 cycles

LEFT SIDE WINDOW HEAT INOP. TRANSFERRED TO MDDR # 117627 AS PER MEL 30-40-01-02 CAT C LP 1076367: REPAIRED BROKEN WIRE AT L2 WINDOW C/P IAW SWPM 20-10-11. OPS CHECK NORMAL. MDDR 117627 CLEARED. PLACARD REMOVED AND MCC NOTIFIED.

Part: PRESSURE SWITCH — LEAKING (NR 2 ENGINE) · airframe 86,126 hrs · 24,682 cycles

#2 ENGINE FUEL PRESSURE SWITCH IS LEAKING FROM FWD FITTING LOCATED ABOVE FUEL FILTER. REMOVED AND REPLACED #2 ENGINE FUEL PRESSURE SWITCH PACKING, AND RE-INSTALLED #2 ENG FUEL PRESSURE SWITCH IAW AMM 73-34-01. PENDING LEAK CHECK. PERFORMED LEAK CHECK IAW AMM 71-00-00, NO LEAKS NOTED.

Part: RELIEF VALVE — FAILED (BLEED AIR SYS) · airframe 86,126 hrs · 24,682 cycles

#1 ENG PRV VALVE HAS FAILED HEALTH CHECK. REMOVED & REPLACED #1 ENG PRV VALVE IAW AMM 36-11-18. OPS CHECK GOOD, NO LEAK NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 86,098 hrs · 24,677 cycles

AFTER TAKEOFF, "FWD EQPT OVHT" EICAS MESSAGE ILLUMINATED. RAN QRH WHICH CALLED FOR PUTTING EQUIP COOLING SELECTOR TO STBY. EICAS MSG EXTINGUISHED. LEFT EQUIPMENT COOLING SELECTOR IN STANDBY PER QRH.&NBSP;(<P>TROUBLESHOT PER FIM 21-58 FAULT TREE 912. NO MESSAGES SHOWN. CLEANED SUPPLY EXHAUST FAN SCREEN PER AMM 21-58-22.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 85,998 hrs · 24,657 cycles

EICAS MSG OF "FWD EQPT OVHT" RCVD DURING INITIAL CLIMB. EICAS MSG CLEARED AFTER COMPLETING STEP 6 OF NNC. PERFORMED OPS CHECK OF FWD EQPT COOLING SYSTEM GRILL INLET, SUPPLY AIR INLET, EXHAUST FAN, AND SCREEN. OPS CHECKED GOOD AT THIS TIME PER AMM 21-58-00/201.

Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 85,785 hrs · 24,611 cycles

#1 EQUPIMENT COOLING FAN EICAS MESSAGE DISPLAYED &AMP; CB POPPED. (<P>REMOVED AND REPLACED&NBSP;#1 EQUIPMENT COOLING FAN IAW AMM 21-26-01-004-001/404-024, OPS CHECK GOOD.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,729 hrs · 24,600 cycles

LT PACK TEMP&NBSP; DISPLAYED ON APPROACH LIGHT EXTINGUISHED&NBSP; AND CAME BACK ON&NBSP;(<P>PERFORMED&NBSP; LEFT PACK TEMP CONTROLLER PER AMM 21-51-14 OPS CHECK OK</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 85,688 hrs · 24,594 cycles

WX RADAR REQUIRES -6 TILT TO SEE T-STORMS 40 NM AWAY. (<P>PERFORMED OPS CHECK OF WEATHER RADAR AS PER AMM 34-43-00. OPS CHECKED GOOD AT THIS TIME.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIPMENT OVERHE) · airframe 85,564 hrs · 24,570 cycles

ON CLIMBOUT @ APPROX 2000' AGL, EICAS MSG FWD EQPT OVHT, FOLLOWED QRH AND MESSAGE CLEARED. OPS TEST C/W IAW AMM 21-58-00, ALL TEST PASS. NO ACTIVE MSG AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 85,522 hrs · 24,559 cycles

EQUIPMENT COOLING EICAS DID NOT RESOLVE. OPERATED IN STANDBY MODE PER QRH, MESSAGE STAYED CLEAR W STDBY MODE. PERFORMED OPERATIONAL TEST IAW AMM 21-58-00. OPS CHECKS GOOD.

Part: WINDOW — DAMAGED (L3) · airframe 85,499 hrs · 24,553 cycles

L3 WINDOW HAS BUBBLES. REMOVED AND REPLACED L3 WINDOW IAW AMM 56-11-00-404. ACCOMPLISHED L3 WINDOW HEAT SYSTEM CHECK PER AMM 30-41-00, TEST GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 85,481 hrs · 24,548 cycles

AFTER T/O, CLIMBING 1000 FT, EICAS MSG "FWD EQUIPMENT OVHT". IAW QRH UP TO STEP 7, EICAS MSG CLEARED. NO STATUS MSG. OPS TEST CARRIED OUT IAW AMM 21-58-00. ALL TEST PASS, NO ACTIVE MSGS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,475 hrs · 24,547 cycles

ON INSPECTION, FOUND FLT DECK EMERGENCY EXIT LIGHT INOP. OPERATIONAL CHECK OK IAW B767 AMM 33-51-00-715-200.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,475 hrs · 24,547 cycles

ON INSPECTION, FOUND LEFT &AMP; RIGHT OVER WING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW B767 AMM 33-51-07. EMERGENCY EXIT LIGHTS OPS CHECK NORMAL IAW B767 AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,475 hrs · 24,547 cycles

ON INSPECTION, FOUND LEFT EXT EMERGENCY 2 AFT LIGHTS INOP.(<P>REPLACED BULBS FOR LEFT AFT EXT EMERGENCY LIGHTS IAW B767 AMM 33-51-01. OPS CHECK NORMAL.</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 85,372 hrs · 24,525 cycles

CENTER LEFT FUEL PUMP MESSAGE ON CLIMB OUT.(<P>TRANSFERRED CENTER LEFT FUEL PUMP TO MDDR #111904 PER MEL 28-22-02A CAT C DUE 29MAY19 PLACARD INSTALLED.</P><P>LP 1081508 - M10: REMOVED AND REPLACED LEFT CENTER BOOST PUMP IAW AMM 28-22-02.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,209 hrs · 24,491 cycles

FLIGHT DECK TEMP EICAS AFTER ENGINE SHUTDOWN(<P>PERFORMED BITE TEST AND FIM TASK PER 21-64. OPS CHECKED GOOD.<BR /></P>)

Part: VALVE — DAMAGED (APU SURGE) · airframe 85,130 hrs · 24,472 cycles

APU SURGE VALVE FILTER THREADS DAMAGED INTERNALLY.(<P>REMOVED AND REPLACED&NBSP;APU SURGE VALVE REF B767 AMM 49-53-01.</P>)

Part: EXHAUST FAN — FAILED (NR 2 AFT) · airframe 85,013 hrs · 24,447 cycles

STATUS MESSAGE AFT EQ EX FAN 2.(<P>REMOVED AND REPLACED #2 AFT EQ EXHAUST FAN ASSY PER AMM 21-26-01.<BR /></P>)

Part: START VALVE — WARNING MESSAGE (RT ENGINE) · airframe 84,983 hrs · 24,441 cycles

EICAS MESSAGES R STARTER CUTOUT AND R ENG STARTER DISPLAYED AFTER TAKEOFF(<P>REMOVED AND REPLACED R ENGINE STARTER VALVE I.A.W 80-11-02. OPS CHECKS GOOD.&NBSP;<BR /></P>)

Part: PIN — DAMAGED (ACTUATOR SQUIB) · airframe 84,945 hrs · 24,432 cycles

DURING DISARM OF OFF WING ESCAPE SYSTEM FOR MAINT. FOUND LH SPOILER OVERRIDE ACTUATOR SQUIB PINS PUNCHED AND BENT. REMOVED AND REPLACED LH SPOILER OVERRIDE ACTUATOR SQUIB IAW AMM 25-65-10. OPS CHECKED GOOD IAW AMM 25-65-00.

Part: FAN — INOPERATIVE (EQUIP EXHAUST) · airframe 84,945 hrs · 24,432 cycles

AFT EQUIPMENT EXHAUST FAN INOP. RESET THE C/B. FLEW 2 LEGS, NO ISSUES IAW 21-58-001.

Part: DUCT — PUNCTURED (SURGE VALVE) · airframe 84,945 hrs · 24,432 cycles

DURING MAINT TASK ON APU, FOUND SURGE CONTROL VALVE RUBBER DUCT WITH HOLE IN IT.(<P>REMOVED AND REPLACED SURGE VALVE DUCT PER AMM 49-53-01. LEAK AND OPS CHECK GOOD.

Part: PACKING — WORN (APU OIL CAP) · airframe 84,945 hrs · 24,432 cycles

APU HAS OIL LEAK IN THE VICINITY OF THE FILL CAP. FOUND OIL CAP PACKINGS WORN. REMOVED AND REPLACED APU OIL TANK CAP PACHINGS PER AMM 12-13-01-613-001. OPERATED APU &AMP; NO LEAKS NOTED.<BR /></P>)

Part: CHECK VALVE — NOT REPORTED (BLEED AIR SYS) · airframe 84,887 hrs · 24,420 cycles

LEFT ISLN CHECK VALVE. CHECK VALVE PN 732-11750-03(<P>R/R ISOLATION BYPASS CHECK VALVES IAW AMM 36-11-05/401. OP PNEUMATIC LEAK NORMAL AT THIS TIME.</P>)

Part: TERMINAL — DEFECTIVE (FIRE LOOP) · airframe 84,765 hrs · 24,397 cycles

LEFT ENGINE LP 1 INOP&NBSP;(<P>TRANSFERRED TO MDDR 108667</P><P>LP 0971739-M6: REPLACED TERMINAL END LEFT ENG UPPER AFT LOOP RIGHT SIDE IAW SWPM 20-10-11. LEFT ENGINE FIRE WARNING CHECKS OK PER AMM 26-11-00. CLOSED MDDR 108667.</P><P><BR /></P>)

Part: INDICATOR — FAILED (COCKPIT) · airframe 84,765 hrs · 24,398 cycles

PER TASK CARD A-77-304-01 TALLY 8027 STANDBY ENGINE INDICATIOR (ETOPS) BITE TEST FAILED(<P>REMOVED AND REPLACED STANDBY ENGINE INDICATOR IAW AMM 77-41-01. BITE TEST SATISFACTORY IAW 77-41-01.</P>)

Part: ACOUSTIC LINER — DELAMINATED (NR 1 ENGINE) · airframe 84,765 hrs · 24,398 cycles

DURING INSPECTION ON NR 1 ENGINE ACCUSTICAL LINER SEGMENT FROM 4 O CLOCK TO 6 O CLOCK POSITION WAS FOUND WITH DELAMINATION.(<P>REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT IAW AMM 72-33-01-004-001-H00 AND 72-33-01-404-011-H00.</P>)

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 84,765 hrs · 24,398 cycles

ENG #2 DURING ACCOMPLISHMENT OF LP COMPRESSOR ROTOR BLADES INSPECTION WERE FOUND SEVERAL BLADES WITH NICKS AND DENTS WITHIN LIMITS THAT WILL NEED BLEND. REPAIRED BLADES ON #2 ENGINE IAW AMM 72-31-02-308-055-H00.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 84,750 hrs · 24,394 cycles

LT PACK INOP IN AUTO(<DIV>R/R LT PACK TEMP CONTROL VALVE PER AMM 21-51-12 OPS CHECKS GOOD. DISPATCH AA@0655Z</DIV>)

Part: LIFE RAFT — OUT OF POSITION (CABIN) · airframe 84,750 hrs · 24,394 cycles

O/H BIN WITH EXTRA LIFE RAFT WONT STAY SHUT(<DIV>REPOSITIONED LIFE RAFT IN OVRHEAD BIN. NOW CLOSES BETTER AND STAYS LOCKED</DIV>)

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 84,713 hrs · 24,387 cycles

LEFT ENGINE LOOP 1 INOP.&NBSP;(<P>DEFERRED IAW MEL 26-11-01-0 CNTRL 18 MAR 19, MDDR #108360.<BR /></P><P>LP 0971727-M20 REMOVED AND REPLACED&NBSP; FIRE DETECTION CARD ASSY IAW AMM 26-10-01, OPS CHECK OK. CLEARED MDDR # 108360.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,681 hrs · 24,381 cycles

LEFT PACK OFF EICAS MESSAGE AFTER ENGINE START.(<DIV>CYCLE PACK SWITCH, CYCLE LEFT ISOLATION VALVE. OPS CHECK GOOD. REF FIM 21-51 FT 876. SYSTEM OK FOR SERVICE.&NBSP;</DIV>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,681 hrs · 24,381 cycles

LEFT FIRE LOOP STATUS MESSAGE.&NBSP;(<P>ENGINE FIRE DETECTION SYSTEM TEST CARRIED OUT IAW AMM 26-11-00 TEST PASS MESSAGE SELF ERASED.&NBSP;</P>)

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 84,603 hrs · 24,366 cycles

L FWD FUEL PUMP EICAS AND PRESS LIGHT ON RADAR DOWNWIND(<P>TRANSFER TO MDDR 107885 IAW DDG 28-22-01</P><P>LP 0975817-M7: REMOVED AND CLEANED PRESSURE SWITCH CONNECTOR. RESET C/B, PERFORMED OPS CHECK IAW AMM 28-22-01. OPS CHECK GOOD AND PLACARDS REMOVED. MDDR 107885 CLOSED. DISPATCH @ST10131.&NBSP;</P>)

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 84,574 hrs · 24,360 cycles

OUTFLOW VALVE INDICATION. REMOVED AND REPLACED THE OUTFLOW VALVE ACTUATOR IAW AMM 21-31-04, OPS CHECKED GOOD.

Part: PUMP — INOPERATIVE (FUEL) · airframe 84,516 hrs · 24,347 cycles

L FWD FUEL PUMP INOP(<P>TRANSFER TO MDDR # 107464 IAW DDG 28-22-01 CAT C DUE DATE 02-27-2019</P><P>LP 1054875: REMOVED AND REPLACED LEFT FWD FUEL PUMP IAW AMM 28-22-03, OPS CHECKED GOOD. THIS CLEARS MDDR 107464. PLACARD REMOVED.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 84,516 hrs · 24,347 cycles

ON FINAL APP, L FWD FUEL PUMP EICAS WITH 11.0 IN L FUEL TANK&NBSP;(<P>OPERATED LT FWD FUEL PUMP SW, ALL EICAS AND LOW PRESSURE LIGHTS FUNCTION NORMAL PER AMM 28-42-01</P>)

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 84,467 hrs · 24,336 cycles

"RT AFT FUEL PUMP LOW PRESS SWITCH INOP / ( FUEL PUMP LOW PRESS LIGHTS, -200/-300 )"(<P>R/R RIGHT AFT FUEL PRESS SWITCH PER AMM 28-42-01,THIS CLEARS MDDR 107124.</P>)

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 84,467 hrs · 24,336 cycles

"L FWD FUEL PUMP INOP / ( MAIN TANK FUEL PUMPS (NOTIFY DISPATCH)."(<P>REMOVE AND REPLACED PRESSURE SWITCH IAW 28-42-01,THIS CLEARS MDDR 107070.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 84,428 hrs · 24,328 cycles

L FORWARD FUEL PUMP EICAS MSG&NBSP;(<P>PERFORMED OPS TEST OF LEFT FORWARD FUEL PUMP, ALL CHECKS OK NO FAULTS OR EICAS MSG AS PER AMM 28-22-00</P>)

Part: WIRE — BROKEN (RT ENG PRV) · airframe 84,366 hrs · 24,313 cycles

R ENG PRV EICAS RECEIVED IN FLIGHT&NBSP;(<P>TRANSFERRED TO MDDR # 106721 AS PER MEL 36-11-08-01-01A CAT C&NBSP;</P><P>FOUND OPEN BETWEEN AIR SUPPLY BITE MODULE D2378A-B13 AND PIN 1 OF PRV CONTROLLER CAUSED BY BROKEN WIRE AT TB320 YA19 AT P37 PANEL , RESECURED WIRE AT TB320 YA19 PER SWPM 20-90-11 RAN ENG AND OPS CHECK OK, MDDR CLOSED&NBSP;<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 84,304 hrs · 24,298 cycles

RT ENG PRV EICAS AFTER ENG START(<P>TRANSFERRED TO MDDR 106393 IAW DDG 36-11-08-01-01A</P><P>REF LOG PAGE 1025719 ITEM M3; REMOVED AND REPLACED RIGHT ENGINE PRV IAW AMM 36-11-18. OPS CHECK NORMAL. NO LEAKS NOTED. LOG PAGE 1025720 ITEM M4; REMOVED AND REPALCED PRESSURE REGULATING CONTROLLER ASSY IAW AMM 36-11-19/401, OPS CHECK OK, NO LEAKS FOUND, NO EICAS MESSAGE AFTER ENGINE RUN LEAK CHECK. THIS CLEARS MDDR 106393.&NBSP;<BR DATA-MCE-BOGUS="1" /></P><P>PRV P/N 802170-12&NBSP; S/N 200103159</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 84,218 hrs · 24,276 cycles

AFTER ENG SHUTDOWN LEFT ENGINE ANTI ICE VALVE FAILED TO CLOSE&NBSP;(<P>REMOVED AND REPLACED LEFT ENGINE&NBSP; NOSE ANTI ICE VALVE IAW AMM 30-21-03 OPERATIONAL TEST OK</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 84,241 hrs · 24,281 cycles

RIGHT FWD FUEL PUMP SWITCH WHEN TURNED OFF, NO PRESS LIGHT AND NO R FWD FUEL PUMP EICAS MSG.(<P>REPLACED THE RIGHT FWD FUEL PUMP PRESSURE SWITCH, REF AMM 28-42-01 MDF 2668639 OPS AND LEAK NORMAL.<BR /></P>)

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 84,210 hrs · 24,275 cycles

LEFT FWD FUEL PRESSURE LIGHT WILL NOT EXTINGUISH WITH APU RUNNING.(<P>FWD TO MDDR 105784 PER MEL 28-42-01-01 CAT C. DUE DATE 21JAN19. ORANGE PLACARD INSTALLED. DISPATCH: @ 1309Z.LOG PAGE&NBSP; 0978492-M11 REMOVED AND REPLACED LEFT FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01 OPS CHECK AND LEAKS NORMAL THIS CLEARED DMI 105784&NBSP;</P>)

Part: TRANSCEIVER — DEFECTIVE (WEATHER RADAR) · airframe 84,177 hrs · 24,266 cycles

RIGHT SIDE WX RADAR SYS DISPLAYS MSG WXR WEAK. (<P>R/R WEATHER RADAR RT SIDE REF AMM 34-43-01 OPS CK OK<BR /></P>)

Part: FIRE DETECTOR — FAULTY (LT ENGINE) · airframe 84,177 hrs · 24,266 cycles

L ENG FIRE LP 2 STATUS MSG. (<P>R/R L ENG FIRE UPPER AFT DETECTOR&NBSP; REF AMM 26-11-01<BR /></P>)

Part: STRUCTURE — CORRODED (FILL PORT) · airframe 84,175 hrs · 24,265 cycles

LEFT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18210 IR.</P>)

Part: LINE — LEAKING (NR 1 ENG PRV) · airframe 84,175 hrs · 24,265 cycles

#1 ENG PRV SENSE LINE/ELBOW @PRV IS LEAKING DAMAGED/LEAKS.(<P>REMOVED AND REPLACED #1 ENG SENSE LINE AND ELBOW @ PRV IAW N767 AMM 36-11-18. ELBOW P/N AS4138J0608.</P>)

Part: WIRE HARNESS — ARCED (FUEL QTY) · airframe 84,175 hrs · 24,265 cycles

CUSTOMER REQUEST:RIGHT WING FUEL QUANTITY WIRE HARNESS SHOWS SIGNS OF ARCING.(<P>REMOVED AND REPLACED R/H FQIS WIRE HARNESS,LEAK CHECK &AMP; BITE CHECK GOOD NO LEAKS NOTED IAW B-767 AMM 28-41-01.</P>)

Part: SENSOR — READS HIGH · airframe 84,175 hrs · 24,265 cycles

ASM HEALTH TEST FAILURE R/H PRESSURE SENSOR OUTPUT IS TO HIGH.(<P>REMOVED AND REPLACED #2 ENG F.A.M.V. TEMP SENSOR IAW B767 AMM 36-11-17.PERFORMED SATISFACTORY LEAK CHECK (NO LEAKS NOTED)IAW B767 AMM 36-11-17.</P>)

Part: VALVE — FAILED (RIGHT) · airframe 84,175 hrs · 24,265 cycles

ASM HEALTH TEST FAILURE R/H FAV OPEN AND CLOSE DISAGREE.(<P>REMOVED AND REPLACED #2 ENG FAV IAW B767 AMM 36-11-16.PERFORMED SATISFACTORY OP/LK CHECK IAW B767 AMM 36-11-16.(NO DEFECTS NOTED).</P>)

Part: SENSOR — MALFUNCTIONED (LEFT) · airframe 84,175 hrs · 24,265 cycles

ASM HEALTH TEST FAILURE L/H F.A.T.S. DOES NOT COMMAND FAV TO CLOSE.(<P>REMOVED AND REPLACED L/H FAN AIR TEMPERATURE SENSOR IAW B767 AMM 36-11-17 OP/LK CHECK ACCOMPLISHED ON WORK T/C 6736A013PT1.</P>)

Part: VALVE — STICKING (NR 1 ENGINE) · airframe 84,175 hrs · 24,265 cycles

#1 ENG. PRV IS STICKING MANUALLY OPEN OR CLOSE.(<P>REMOVED AND REPLACED #1 ENG PRV IAW B767 AMM 36-11-18.ACCOMPLISHED OP/LK CHECK ON WORKSHEET T/C T2031 AND W/C 6736A013PT1.</P>)

Part: STRUCTURE — CORRODED (RT WG FILL PORT) · airframe 84,175 hrs · 24,265 cycles

RIGHT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18207 RIR.</P>)

Part: SPINNER — WORN (NR 1 ENGINE) · airframe 84,175 hrs · 24,265 cycles

#1 ENG SPINNER NEEDS REPAINT AS PER CUSTOMER.(<P>REMOVED,PAINTED &AMP; REINSTALLED #1 ENG SPINNER IAW B767 AMM 72-31-01 &AMP; ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)

Part: WIRE — ARCED (R1 WINDSHIELD) · airframe 84,175 hrs · 24,265 cycles

FLIGHT DECK R-1 WINDSHIELD UPPER AND LOWER ELECTRICAL WIRE STRIPS ARE BROWN FROM ARCING.(<P>REMOVED AND REPLACED FLIGHT DECK R-1 WINDOW WITH SERVICEABLE UNIT IAW B767-3 AMM 56-11-01</P>)

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 84,175 hrs · 24,265 cycles

FWD CARGO BALLMAT HAS CORROSION IN BOTTOM SIDE OF PNL 124BXF.(<P>FABRICATED AND INSTALLED 1EA FILLER AND 1EA DOUBLER REPAIR.</P>)

Part: SEAT TRACK — GOUGED (COCKPIT) · airframe 84,175 hrs · 24,265 cycles

CAPT. SIDE I/B AFT SEAT TRACK HAS GOUGE.(<P>REMOVED AND REPLACED SEAT TRACK.</P>)

Part: RETAINER — MISSING (LT OVRWG HATCH) · airframe 84,175 hrs · 24,265 cycles

L/H FWD OVERWING-EMERGENCY HATCH BOTTOM AFT STOP FTG HAS MISSING STOP PIN RETAINER.(<P>INSTALLED MISSING STOP PIN RETAINER ON L/H FWD OVERWING EMERGENCY HATCH BOTTOM AFT STOP FTG,IAW B-767 AMM 52-21-01,PERFORMED TOLERANCE CHECK OF EMERGENCY HATCH IAW B-767 AMM 52-21-01</P>)

Part: VALVE — INOPERATIVE (RIGHT) · airframe 84,175 hrs · 24,265 cycles

ASM HEALTH TEST FAILURE RIGHT PRV DOES NOT OPEN.(<P>REMOVED AND REPLACED #2 ENG. PRV IAW B767 AMM 36-11-18.PERFORMED SATISFACTORY LEAK CHECK AND NO LEAKS NOTED IAW B767 AMM 36-11-18.</P>)

Part: SENSOR — FAILED (A/C PACK TEMP) · airframe 84,175 hrs · 24,265 cycles

STANDBY PACK TEMP CONTROLLER FAIL AT POSITION 7.(<P>REMOVED AND REPLACED R/H PACK COMPRESSOR OULET SENSOR T55135 IAW B767 AMM 21-51-14.PERFORMED SATISFACTORY PACK STANDBY CONTROLLER BITE TEST IAW B767 AMM 21-51-14.</P>)

Part: IMPELLER — BROKEN (RT COOLING FAN) · airframe 84,175 hrs · 24,265 cycles

R/H E&AMP;E COOLING EXHAUST FAN HAS A BROKEN IMPELLER BLADE.(<P>REMOVED AND REPLACED R/H E&AMP;E BAY EXHAUST FAN IAW B767 AMM 21-58-06.OP/LK CHECK C/W AND NO DEFECTS NOTED IAW B767 AMM 21-58-06.</P>)

Part: SPINNER — WORN (NR 2 ENGINE) · airframe 84,175 hrs · 24,265 cycles

#2 ENGINE SPINNER REQ REPAINT AS PER CUSTOMER REQ.(<P>REMOVED,PAINTED &AMP; REINSTALLED #2 ENGINE SPINNER IAW B767 AMM 72-31-01 &AMP; ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)

Part: SEAT TRACK — GOUGED (COCKPIT) · airframe 84,175 hrs · 24,265 cycles

F/O SIDE I/B AFT SEAT TRACK HAS GOUGE.(<P>REMOVED AND REPLACED SEAT TRACK.</P>)

Part: BATTERY — DISCHARGED (MAIN) · airframe 84,172 hrs · 24,264 cycles

MAIN SHIPS BATTERY IS DEAD. REMOVED AND REPLACED BATTERY IAW AMM 24-31-01 OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,158 hrs · 24,261 cycles

"FWD EQPT OVHT" EICAS. RAN QRH, EQUIPMENT COOLING OPERATIONAL TEST CARRIED OUT IAW AMM 21-58-00. OPS CHK SATIS. NO FAULTS MSGS.

Part: IGNITER — INOPERATIVE (RT ENGINE) · airframe 84,093 hrs · 24,247 cycles

RT ENG IGNITION 1 INOP. REMOVED AND REPLACED RT ENG IGNITOR PLUG 1 AS PER AMM 74-21-02, RAN ENG OPS CHECK OK.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,024 hrs · 24,235 cycles

APU AUTO SHUT DOWN. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05 OPS AND BITE TEST GOOD.

Part: ECU — FAULTY (APU) · airframe 84,044 hrs · 24,239 cycles

APU AUTO SHUTDOWN SEVERAL TIMES, TROUBLESHOOT. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. OPS AND BITE TEST GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,809 hrs · 24,186 cycles

EMERGENCY FLOOR LIGHT FWD OF 20F INOP. R&R LT FLOOR LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,809 hrs · 24,186 cycles

EMERGENCY FLOOR LIGHT FWD OF 20F INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECK OK IAW AMM 33-51-05.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,686 hrs · 24,157 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE FROM SEATS 31C TO 38C. REPLACED THE LAMPS IAW AMM 33-51-05-002-034, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,686 hrs · 24,157 cycles

FLOOR EMERGENCY LIGHT FORWARD OF SEAT 4J INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-10- 912-064.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,686 hrs · 24,157 cycles

FLOOR EMERGENCY LIGHT AFT OF SEAT 19H WAS FOUND INOPERATIVE. REPLACED THE LAMP, AND OPS CHECKED GOOD IAW AMM 33-11-10-962-064.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,686 hrs · 24,157 cycles

EMERGENCY LIGHT INOPERATIVE ABOVE SEAT 33C. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-51-05-002-039.

Part: COVER — DAMAGED (DOOR SLIDE) · airframe 8,368,608 hrs · 24,157 cycles

AFT SERVICE DOOR EMERGENCY SLIDE BUSTLE COVER HAS A LATCH WITH DISBOUNDED INSERTS AT THE FWD BOTTOM LATCH. REPAIRED THE SLIDE BUSTLE COVER LATCH INSERTS IAW AMM 25-00-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,686 hrs · 24,157 cycles

FLOOR EMERGENCY LIGHT, AFT RIGHT SIDE OF FWD COAT CLOSET WAS FOUND INOPERATIVE. RELAMPED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-10-962-054.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,686 hrs · 24,157 cycles

AFT RIGHT EXTERNAL ESCAPE HATCH EMERGENCY SLIDE LIGHT INOPERATIVE. TROUBLESHOT IAW FIM 33-51, FOUND THE BATTERY PACK M733 INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-07-201. OPS CHECKED GOOD IAW AMM 33-51-07-422-012.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYSTEM) · airframe 83,631 hrs · 24,144 cycles

RIGHT WEATHER RADAR SYSTEM INOPERATIVE. R & R THE RIGHT WEATHER RADAR R/T, OPS NORMAL IAW AMM 34-43-00.

Part: WARNING MESSAGE — ILLUMINATED · airframe 83,340 hrs · 24,081 cycles

EICAS IDLE DISAGREE.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E COOLING) · airframe 83,318 hrs · 24,076 cycles

FWD EQUIPMENT COOLING EICAS MESSAGE, SWITCH REMAINED IN STBY FOR REMAINDER OF CHECK FLIGHT. PERFORMED EQUIPMENT COOLING TEST IAW AMM 21-58-00, TESTED OK, NO FUTHER ISSUES.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 83,261 hrs · 24,056 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 20J. INSTALLED A NEW LENS IAW AMM 38-51-10, CHECKED NORMAL.

Part: CIRCUIT CARD — MALFUNCTIONED (ENGINE) · airframe 83,263 hrs · 24,057 cycles

AFTER ENGINE START RECEIVED AN EICAS MESSAGE FOR IDLE DISAGREE. REMOVED AND REPLACED THE M644 CARD IAW AMM 73-21-11. OPS CHECKED OK.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 82,331 hrs · 24,050 cycles

AFTER LANDING, AN IDLE DISAGREE MESSAGE ILLUMINATED. THE RT ADC WAS REPLACED, NO DEFECT NOTED AFTER PERFORMED 30 TEST.

Part: ANTI-ICE VALVE — SLOW (RT ENGINE) · airframe 83,225 hrs · 24,048 cycles

RIGHT ENGINE NOSE ANTI-ICE VALVE SLOW TO CLOSE. REMOVED AND REPLACED THE RT INLET ANTI-ICE VALVE IAWAMM 30-21-03, RAN ENGINE, OPS AND LEAK CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 83,278 hrs · 24,062 cycles

EMERGENCY LIGHT FOUND BROKEN, LENS WILL NOT STAY ON. SECURED THE LENS AT SEAT 19L IAW AMM 20-60-00, OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (BOOST PUMP) · airframe 83,166 hrs · 24,036 cycles

LEFT FWD BOOST PUMP PRESSURE LIGHT WILL NOT GO OUT. : R & R THE LEFT FWD BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01, LEAK AND OPS CHECKED GOOD,

Part: ANTI-ICE VALVE — SLOW (RT ENGINE) · airframe 83,192 hrs · 24,040 cycles

RT ENGINE ANTI-ICE VALVE SLOW TO CYCLE. PERFORMED OPS CHECKED THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED GOOD IAW AMM 30-21-03.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 83,174 hrs · 24,037 cycles

EICAS MESSAGE FOR THE ENGINE ANTI-ICE SYSTEM. PERFORMED OPS CHECK OF THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED OK IAW AMM 30-21-03.

Part: WARNING LIGHT — ILLUMINATED (BOOST PUMP) · airframe 83,166 hrs · 24,035 cycles

LEFT FWD BOOST PUMP PRESSURE LIGHT WILL NOT GO OUT. OPEN

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 83,209 hrs · 24,045 cycles

IDLE DISAGREE MESSAGE AT DEPARTURE. REMOVED AND REPLACED THE LT ADC IAW AMM 34-12-01, OPS CHECK GOOD IAW AMM 34-12-01

Part: WARNING MESSAGE — ILLUMINATED (ENGINE) · airframe 83,150 hrs · 24,032 cycles

IDLE DISAGREE DURING DEPARTURE.

Part: TRANSDUCER — MALFUNCTIONED (THRUST REVERSER) · airframe 83,194 hrs · 24,041 cycles

IDLE DISAGREE AFTER THRUST REVERSER STOWED. R & R THE RT ENG INBD THRUST REVERSER CDU POSITION TRANSDUCER IAW AMM 78-31-24, OPS CHECKED GOOD

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 83,137 hrs · 24,030 cycles

RIGHT ENGINE SHOWED A FAN VIBRATION UP TO 5 DURING TAKEOFF. REMOVED AND REPLACED THE NR 2 ENGINE 5 AND 6 BLADES IAW AMM 72-31-02.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 83,137 hrs · 24,030 cycles

NR 2 ENGINE BLADES 5 AND 6 ARE DAMAGED. R & R THE BLADES. OPS CHECKED NORMAL IAW AMM 72-31-02.

Part: BLADE — DAMAGED (NR 3 FAN) · airframe 83,137 hrs · 24,030 cycles

DURING TAKEOFF, A 4.9 VIBRATION ON FAN. REMOVED AND REPLACED THE NR 3 FAN BLADE IAW AMM 72-31-02 , TRIMMED VIBRATION IAW AMM 72-31-00, TRIM NOW 1.0 AT TAKEOFF, FAN LUBE COMPLIED WITH.

Part: HMU — MALFUNCTIONED (NR 1 ENGINE) · airframe 83,137 hrs · 24,030 cycles

IDLE DISAGREE MESSAGE, AT FLT IDLE AFTER STOWING THE THRUST REVERSER. R & R THE HMU IAW AMM 73-21-14. OPS CHECKED NORMAL IAW AMM 71-00-00.

Part: SPRING — DAMAGED (APU VALVE) · airframe 83,137 hrs · 24,030 cycles

APU BLEED SURGES, VALVE FILTER SPRING IS DAMAGED. R & R APU BLEED SURGE VALVE SPRING. OPS CHECKED NORMAL AND NO LEAKS IAW AMM 49-53-06.

Part: BLADE — DAMAGED (HPC) · airframe 83,137 hrs · 24,030 cycles

NR 2 ENGINE, ONE HPC STAGE 1 BLADE WITH A L/E DENT AND CRACK. BORO BLENDED REPAIR TO THE BLADE IAW AMM 72-00-00.

Part: BOLT — SHEARED (NR 1 ENGINE) · airframe 83,137 hrs · 24,030 cycles

NR 1 ENGINE INBD LOCKOUT PLATE HAS A SHEARED BOLT. R & R THE BOLT IAW AMM 51-40-02.

Part: HMU — MALFUNCTIONED (ENGINE) · airframe 83,048 hrs · 24,012 cycles

IDLE DISAGREE EICAS MESSAGE ON LANDING. RT PIMU HAS A DISAGREE MESSAGE ON BOTH A & B CHANNELS. REMOVED AND REPLACED THE HMU. TESTED 3,2,6 AND 7 IAW AMM 71-00-00, CHECKED OK.

Part: PRINTED CKT BOARD — DEFECTIVE (EEC) · airframe 83,009 hrs · 24,001 cycles

CAUTION MSG IDLE DISAGREE AFTER LANDED RIGHT ENGINE 34.7 N1 LEFT ENGINE 25.5 N1. REMOVED AND REPLACED EEC DISCRETE PRINTED CIRCUIT CARD IAW AMM 73-21-12.

Part: ENGINE — VIBRATION (LEFT) · airframe 82,957 hrs · 23,993 cycles

LEFT ENGINE VIBRATION, 5.0 DURING CLIMB. ADJUSTED THE NR 1 ENGINE FAN TRIM BALANCE USING EXTERNAL ANALYZER IAW AMM 72-31-00/501.

Part: RELAY — MALFUNCTIONED (RT ENGINE) · airframe 82,957 hrs · 23,993 cycles

RIGHT ENGINE IDLE DISAGREE ILLUMINATED AFTER LANDING. REMOVED AND REPLACED THE RT ENGINE REVERSE RELAYS IAW WDM 73-21-19 & 77-35-11 , OPERATED THE ENGINE IAW AMM 71-00-00, OPS CHECKED GOOD, AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,903 hrs · 23,978 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE. PINNED THE LIGHTS IAW AMM 33-51-10, OPS CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 82,903 hrs · 23,978 cycles

SEATS 37J, 32C, FWD OF 19D, EMERGENCY LIGHT LENSES ARE MISSING. REPLACED EMERGENCY LIGHTS LENSES IAW MM 33-53-00.

Part: ACTUATOR — MALFUNCTIONED (SPAR VALVE LIGHT) · airframe 82,903 hrs · 23,978 cycles

LEFT ENGINE SPAR LIGHT VALVE VERY SLOW TO EXTINGUISH IN START AND SHUTDOWN. REMOVED AND REPLACED FUEL SHUTOFF VALVE ACTUATOR IAW MM 28-22-11, OPS CHECKED OK.

Part: RELAY — MALFUNCTIONED (RT ENGINE) · airframe 82,865 hrs · 23,967 cycles

IDLE DISAGREE ON LANDING AFTER REVERSER DEPLOYMENT. REVERSER STOWED NORMALLY. NR 1 IDLE N1 AT 25.5%, NR 2 IDLE 34.8%. REMOVED AND REPLACED THE AIR GROUND RELAY K207 IAW AMM 32-09-02, AND THE RT IDLE SOLENOID RELAY K433 IAW AMM 20-81-00 , RAN ENGINE, OPS CHECKED OK IAW AMM 71-00-00.

Part: LOCK — MALFUNCTIONED (THRUST REVERSER) · airframe 82,689 hrs · 23,935 cycles

IDLE DISAGREE EICAS CAUTION DURING LANDING. REPLACED THE RIGHT ENGINE THRUST REVERSER INBD ELECTRO MECHANICAL BREAK LOCK IAW AMM 78-34-07. OPS CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (FUEL SHUTOFF) · airframe 82,903 hrs · 23,978 cycles

LEFT ENGINE SPAR LIGHT VALVE VERY SLOW TO EXTINGUISH IN START OR SHUTDOWN. REMOVED AND REPLACED THE LEFT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,539 hrs · 23,903 cycles

L4 EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,539 hrs · 23,903 cycles

LT FUSELAGE AFT OF LEFT WING EMERG LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-16.

Part: START VALVE — FAILED (LEFT) · airframe 82,550 hrs · 23,906 cycles

LEFT STARTER CUTOUT CAUTION MESSAGE AT 18,000 FT DURING CLIMB. COMPLIED WITH THE QRH, THE MESSAGE REMAINED. REMOVED AND REPLACED THE LEFT ENGINE START VALVE IAW AMM 80-11-02. OPS AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (BOOST PUMP) · airframe 82,495 hrs · 23,894 cycles

EICAS MESSAGE FOR THE LT FWD FUEL PUMP. PERFORMED A PUMP TEST IAW AMM 28-22-00-215-018. TESTED OK. NO OTHER FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL INDICATOR) · airframe 82,499 hrs · 23,895 cycles

EICAS MESSAGE FOR INTERMITTANT FUEL CONFIGURATION LEFT FUEL GAUGE BLANKED, THEN READ 3000 LBS HIGH BEFORE RETURNS TO NORMAL STATUS MESSAGE. FUEL QTY CHANNEL. PERFORMED TASK 24-41 TREE 837, TESTED OK. PERFORMED QUANTITY TEST IAW AMM 28-41-00-715-031-001. TESTED OK. NO OTHER FAULTS.

Part: WINDOW — ARCED (R2) · airframe 82,499 hrs · 23,895 cycles

R2 SLIDING WINDOW ARCING, IN THE AFT LOWER CORNER. REMOVED AND REPLACED THE R2 SLIDING WINDOW IAW AMM 56-11-03.

Part: LIGHT — UNKNOWN (EXTERIOR) · airframe 82,499 hrs · 23,895 cycles

LEFT SIDE EXTERIOR EMERGENCY LIGHT, LEFT WING SLIDE INOPERATIVE. PERFORMED A CHECK OF EXTERIOR EMERGENCY LIGHTS. OPS CHECKED OK. IAW AMM 33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,455 hrs · 23,886 cycles

RT ISLE OVERHEAD EMERGENCY LIGHT LENS MISSING AT ROW 12. INSTALLED THE LENS IAW AMM 33-21-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG BLEED) · airframe 82,457 hrs · 23,887 cycles

AFTER LANDING, A LT ENGINE BLEED OFF MESSAGE ACTIVATED. PERFORMED AN AIR SUPPLY BITE IAW 36-20-00, NO FAULTS. OPERATED LEFT ENGINE IAW 71-01-02, BLEEDS OPS CHECKED GOOD.

Part: ECU — FAILED (ENGINE) · airframe 82,406 hrs · 23,878 cycles

AFTER ENGINE START , IDLE DISAGREE EICAS MESSAGE. REMOVED AND REPLACED ECU. OPS CHECKED NORMAL IAW AMM 73-21-15.

Part: RELAY — FAILED (RT ENGINE) · airframe 82,406 hrs · 23,878 cycles

RT ENGINE GOING TO FLT IDLE AFTER START. REMOVED AND REPLACED THE IDLE RELAY K433 IAW WDM 20-60-04. ENGINE RUNS CARRIED OUT IAW AMM 71-01-02, OPS CHECKED NORMAL.

Part: PUMP — FAILED (FUEL BOOST) · airframe 82,455 hrs · 23,886 cycles

AFTER FUEL XFEED L - R , RE-SELECTED R PUMPS ON, XFEED ON , EICAS R AFT FUEL PUMP W/ PRESS LT IN SWITCH&NBSP;(<P>REMOVED AND REPLACED RH AFT MAIN BOOST PUMP AS PER AMM 28-22-03 OPS CHECK GOOD, NO FURTHER DEFECTS NOTED&NBSP;</P>)

Part: RELAY — MALFUNCTIONED (RT ENGINE) · airframe 82,361 hrs · 23,871 cycles

AFTER TOUCH DOWN, THE RT ENGINE REMAINED IN HIGH IDLE, N1 34%, N2 75% AND RECEIVED IDLE DISAGREE MESSAGE, INSPECTED ,CLEANED AND INSTALLED THE RELAY K433 IAW AMM 20-60-04. ENGINE RUNS IAW AMM 71-01-02. CHECKED NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 82,358 hrs · 23,869 cycles

DURING THE NR 2 ENGINE START, THE ENGINE ADVANCED TO 35 PERCENT N1 AND 74 PERCENT N2 ON ITS OWN AND RECEIVED IDLE DISAGREE EICAS. TROUBLESHOT IAW FIM 71-05 F/T 844. PERFORMED ENGINE RUNS IAW AMM 71-01-02. INDICATIONS NORMAL, OK FOR SERVICE.

Part: RADAR — UNKNOWN (WEATHER) · airframe 82,112 hrs · 23,808 cycles

WEATHER RADAR TILT NOT WORKING CORRECTLY. PERFORMED A WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00, OPS CHECKED NORMAL.

Part: RADAR — OUT OF ADJUST (WX SYSTEM) · airframe 82,086 hrs · 23,801 cycles

TILT IS OFF ON RADAR. AT 7000 FT, ZERO TILT, GOOD WEATHER PICTURE. AT FL 380, -1 TILT NO WEATHER RADAR PRINTED. PERFORMED A WEATHER RADAR ADJUSTMENT TEST IAW AMM 34-43-00-501, OPS NORMAL, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 1) · airframe 82,029 hrs · 23,790 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 1. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-51-10, OPS CHECKED GOOD. OK FOR SERVICE.

Part: GENERATOR — TRIPPED (RIGHT) · airframe 81,997 hrs · 23,783 cycles

RT GENERATOR CONTROL TRIPPED AFTER ENGINE START, RESET IAW QRH OPS NORMAL. PERFORMED AN OPS TEST FOR RIGHT IDG IAW AMM 24-11-00-715-006, OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 82,029 hrs · 23,790 cycles

IDLE DISAGREE EICAS CAME ON DURING LANDING. SELF EXTINGUISH DURING TAXI. OPS CHECKED NORMAL IAW FIM 71-05-844.

Part: PITOT HEAD — INOPERATIVE (FIRST OFFICER'S) · airframe 81,974 hrs · 23,778 cycles

FIRST OFFICER`S PITOT HEAT INOPERATIVE. REMOVED AND REPLACED THE PITOT TUBE IAW AMM 34011-01, OPS AND LEAK CHECKED GOOD IAW 34-11-00-501, NO LEAKS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,984 hrs · 23,780 cycles

IDLE DISAGREE EICAS MESSAGE ON LANDING. IAW AMM 77-12-00 NO FAULTS NOTED.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 81,906 hrs · 23,764 cycles

LEFT WEATHER RADAR DURING DESCENT, PAINTED A 15 MILE ARC DURING NUMEROUS HEADING CHANGES , DID NOT TRY THE RT RADAR. PERFORMED A WEATHER RADAR TEST IAW AMM 34-43-00, OPS CHECKED GOOD ON GROUND.

Part: PUMP — WARNING MESSAGE (FUEL SYS) · airframe 81,902 hrs · 23,761 cycles

RT AFT FUEL PUMP EICAS MESSAGE. REMOVED AND REPLACED RIGHT AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: SQUIB — NO TEST (OVERWING SLIDE) · airframe 81,891 hrs · 23,760 cycles

OVERWING SQUIBS WILL NOT TEST. DISARMED AND REARMED THE OVERWING ESCAPE SYSTEM IAW AMM 25-65-00. OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (RT ENGINE) · airframe 81,891 hrs · 23,760 cycles

RIGHT ENGINE IDG OUT TEMP MAINTENANCE MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE AIR SHUTOFF VALVE IAW AMM 24-11-07, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,841 hrs · 23,751 cycles

IDLE DISAGREE EICAS MESSAGE ON LANDING. RAN FIM 22-03 F/T'S 803 & 810, TESTS 2 & 10 ON MCDP. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT IDG TEMP) · airframe 81,827 hrs · 23,747 cycles

RIGHT ENGINE IDG OUT TEMP. RT ENG READING HIGH. PERFORMED 24-26 FAULT TREE 807, OUT TEMP DISPLAY. NO FAULT ON WIRING NOTED. RESISTANCE CHECKED WITHIN LIMITS. OPS CHECKED NORMAL.

Part: HEAT EXCHANGER — LEAKING (LEFT) · airframe 81,818 hrs · 23,745 cycles

LEFT DUCT LEAK AFTER LANDING. REMOVED AND REPLACED THE SECONDARY HEAT EXCHANGER. LEFT SIDE IAW AMM 21-51-02. NO LEAKS, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (IDG) · airframe 81,815 hrs · 23,744 cycles

IDG OUT TEMP MTC MESSAGE, RT ENGINE READING HIGH. CONFIRMED IDG SERVICING IAW AMM 12-13-03, COMPLIED WITH FIM 24-20 FT 807, NO FAULTS NOTED, IDG OK FOR SERVICE.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYSTEM) · airframe 81,768 hrs · 23,734 cycles

APU HAS AN OIL LEAK, FOUND ON POST ACFT POSITIONING WALK AROUND. R & R THE OIL PRESSURE SWITCH IAW AMM 49-94-02, LEAK CHECKED GOOD.

Part: SWITCH — INOPERATIVE (CARGO BAY) · airframe 83,823 hrs · 17,786 cycles

FWD CARGO HEAT OV/HEAT INOP. R&R SWITCH ASSY FOR FWD CARGO HEAT, OPS CKD GOOD PER AMM 33-13-00.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYS) · airframe 81,723 hrs · 23,724 cycles

OIL LEAK FROM THE APU. R & R THE OIL PRESSURE SWITCH, OPS CHECKED GOOD, LEAK CHECKED GOOD IAW AMM 49-94-02.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 81,643 hrs · 23,706 cycles

RIGHT PACK OFF LIGHT WITH ALL OTHER PARAMETERS NORMAL AND PACK RUNNING. REPLACED THE RIGHT PACK FLOW CONTROL VALVE IAW AMM 21-51-01. OPS CHECKED NORMAL.

Part: IDG — MALFUNCTIONED (RT GENERATOR) · airframe 81,631 hrs · 23,704 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE ILLUMINATED AFTER RIGHT ENGINE START AND STAYS ON FOR 2 TO 3 MINUTES. REMOVED AND REPLACED THE RIGHT IDG IAW AMM 24-11-01, ENGINE RUN AND GENERATOR GROUND OPERATIONS NORMAL.

Part: CIRCUIT CARD — FAILED (RT A/C PACK) · airframe 81,620 hrs · 23,701 cycles

RIGHT PACK OFF LIGHT ILLUMINATED. REMOVED AND REPLACED THE RT PACK FLOW CONTROL CARD IAW AMM 21-51-09. OPS CHECKED GOOD.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 81,608 hrs · 23,698 cycles

RIGHT A/C PACK OFF MESSAGE. A/C PACK RESET & BITE TEST CARRIED OUT IAW AMM 21-51-00. NO ACTIVE MESSAGES, OK FOR SERVICE.

Part: ACTUATOR — FAILED (APU INTAKE DOOR) · airframe 81,540 hrs · 23,683 cycles

APU FAILED ON START FIRST ATTEMPT, APU DOOR STATUS MESSAGE. REMOVED AND REPLACED THE AIR INTAKE DOOR ACTUATOR IAW AMM 49-15-06. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CLAMP — LOOSE (DUCT) · airframe 81,516 hrs · 23,676 cycles

RIGHT DUCT LEAK AND ASSOCIATED EICAS MESSAGE DISPLAYED WHEN PARKED ON RAMP , QRH PROCEDURE COMPLIED WITH. FOUND LOOSE CLAMP ON THE RT ISOLATION VALVE , TIGHTEN THE CLAMP IAW AMM 36-11-04, OPS CHECKED SATISFACTORY, NO FURTHER MESSAGES.

Part: APU — MALFUNCTIONED · airframe 81,506 hrs · 23,675 cycles

APU FAILED TO START, 2 ATTEMPTS. APU DOOR STATUS MESSAGE. RESET DOOR INLET CIRCUIT BREAKER & BITE TESTED THE APU ECU IAW AMM 49-61-05. OPS CHECKED SATISFACTORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU DOOR) · airframe 81,540 hrs · 23,683 cycles

APU DOOR MESSAGE SELF ERASED AFTER RESET OF CIRCUIT BREAKER AND BITE TEST OF ECU IAW AMM 49-61-05. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (APU DOOR) · airframe 81,458 hrs · 23,660 cycles

APU WOULD NOT START AFTER FLIGHT , APU DOOR STATUS MESSAGE. FOUND APU DOOR CIRCUIT BREAKER TRIPPED, RESET, STARTED APU SEVERAL TIMES AND CHECKED GOOD IAW AMM 49-41-00</P>)

Part: ACTUATOR — FAILED (APU DOOR) · airframe 81,432 hrs · 23,654 cycles

WHILE ATTEMPTING TO START APU. APU DOOR ACTUATOR CIRCUIT BREAKER TRIPPED. R & R APU DOOR ACTUATOR IAW AMM 49-15-06, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 81,600 hrs · 23,697 cycles

RIGHT PACK OFF MESSAGE. RT PACK RESET & A BITE TEST WAS CARRIED OUT IAW AMM 21-51-01. NO ACTIVE MESSAGES, OK FOR SERVICE.

Part: ISOLATION VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 81,356 hrs · 23,638 cycles

RIGHT BLEED ISLN VAL EICAS CAUTION MSG WHILE STILL ON THE BLOCK. REMOVED AND REPLACED RIGHT ISOLATION VALVE IAW AMM 36-11-04. OPS AND LEAK CHECK GOOD.

Part: CONTROLLER — FALSE INDICATION (L2 WINDOW HEAT) · airframe 81,318 hrs · 23,631 cycles

EICAS MESSAGE FOR THE L2 SIDE WINDOW. QRH PROCEDURES ACCOMPLISHED. REMOVED AND REPLACED LT WINDOW HEAT CONTROLLER IAW AMM 30-41-01, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 81,311 hrs · 23,629 cycles

EICAS MESSAGE FOR THE LT SIDE WINDOW DISPLAYED. ACCOMPLISHED QRH. PERFORMED FIM 30-41 FT 804 AND BITE TEST. HEAT CONTROLLES. NO FAULTS NOTED. WINDOW HEAT OK.

Part: IDG — LOW (RIGHT) · airframe 81,300 hrs · 23,627 cycles

RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED AND SHOWN APPROX FOR 90 SECONDS AFTER ENGINE START. SERVICED THE RT IDG OIL IAW AMM 12-13-03, NO DISCREPANCIES NOTED.

Part: APU — MALFUNCTIONED · airframe 81,318 hrs · 23,631 cycles

APU SHUTDOWN UNCOMMANDED ON RAMP. PERFORMED BITE TEST OF APU CONTROL UNIT IAW AMM 49-61-05, 49-61-05-742-027. NO FAULTS FOUND.

Part: INDICATOR — INOPERATIVE (SPAR VALVE) · airframe 81,265 hrs · 23,620 cycles

LEFT ENGINE SPAR VALVE LIGHT INOPERATIVE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WINDOW) · airframe 81,263 hrs · 23,618 cycles

LEFT SIDE WINDOW EICAS. PERFORMED FIM 30-41 FT 804 &. CHECKED WINDOW HEAT CONTROLLER, NO FAULT NOTED. OPS CHECKED OK.

Part: GCU — UNKNOWN (RIGHT) · airframe 81,254 hrs · 23,617 cycles

REMOVED AND REPLACED RT GENERATOR CONTROL UNIT IAW AMM 24-22-02 OPS CHECK GOOD IAW AMM 71-00-00 NO FUTHER DEFECT NOTED AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (LT WINDOW) · airframe 81,241 hrs · 23,614 cycles

LEFT SIDE WINDOW EICAS MESSAGE DISPLAYED. ACCOMPLISHED QRH, PERFORMED FIM 30-41 FT 804, TASK 802, SWAPPED LT WINDOW NR 3 TO SPARE SENSOR IAW AMM 30-41-00, OPS CHECKED NORMAL AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 81,218 hrs · 23,608 cycles

LEFT SIDE WINDOW EICAS MESSAGE. ACCOMPLISHED QRH. PERFORMED BITE ON THE WINDOW HEAT CONTROLLER, NO FAULTS. WINDOW HEAT CHECKED NORMAL IAW AMM 30-41-01.

Part: WARNING LIGHT — FALSE ACTIVATION (WINDOW) · airframe 81,151 hrs · 23,594 cycles

LEFT SIDE WINDOW CAUTION MESSAGE ON EICAS DURING FLIGHT. WINDOW HEAT CONTROL UNIT BITE TEST CARRIED OUT IAW AMM 30-41-01, NO FAULTS, OK FOR SERVICE.

Part: IDG — UNDERSERVICED (RIGHT) · airframe 81,118 hrs · 23,587 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE, AFTER START. EXTINGUISHED IN 60 SECONDS. PERFORMED A RT IDG OIL SERVICING IAW AMM TASK 12-13-03-613-027.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 81,130 hrs · 23,590 cycles

RT AFT FUEL PUMP MESSAGE DURING FLIGHT, COMPLIED WITH QRH. PERFORMED SYSTEM TEST IAW FIM 28-22-820. NO FAULTS NOTED. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,118 hrs · 23,587 cycles

R AFT FUEL PUMP MSG INFLIGHT C/W QRH, PERFORMED SYSTEM TEST & IAW AMM 28-22-820. NO FAULTS NOTED OK FOR SERVICES.

Part: APU — FAULTED · airframe 81,053 hrs · 23,573 cycles

APU SHUTDOWN WITH A FAULT INDICATION AFTER BLOCK IN. RESTART NORMAL. PERFORMED APU BITE IAW AMM 49-61-05, NO FAULTS INDICATED. PERFORMED START IAW AMM 49-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E OVERHEAT) · airframe 81,028 hrs · 23,567 cycles

DURING CLIMB OUT, THE FWD EQUIPMENT OVERHEAT EICAS MESSAGE ACTIVATED. COMPLETED QRH, MESSAGE DID NOT ILLUMINATE AGAIN. RETURNED EQUIPMENT COOLING SWITCH TO AUTO AND COMPLIED WITH SYSTEM OPS CHECK IAW AMM 21-58-00, NO FAULTS INDICATED.

Part: SHUTOFF VALVE — FAULTED (HEAT EXCHANGER) · airframe 80,997 hrs · 23,559 cycles

RIGHT ENGINE IDG OUT TEMP MAINTENANCE MESSAGE. PERFORMED FIM 24-20 FAULT TREE 807, FOUND IDG AIR/OIL COOLER VALVE TO BE FAULTY, REMOVED AND REPLACED AIR/OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24-11-07. OPS CHECKED NORMAL

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,997 hrs · 23,559 cycles

RIGHT UPPER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-05.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 80,997 hrs · 23,559 cycles

LEFT ROW 4-9 EMERGENCY LIGHT INOPERATIVE. INSTALLED THE CONNECTORS IAW AMM 33-51-10. OPS CHECKED NORMAL.

Part: IDG — FAILED (RT ENGINE) · airframe 80,997 hrs · 23,559 cycles

MESSAGE FOR THE IDG OUT TEMP RT ENG. REMOVED AND REPLACED THE IDG IAW AMM 24-11-01. OPS CHECKED NORMAL.

Part: SPRING — MISSING (SURGE VALVE) · airframe 80,997 hrs · 23,559 cycles

APU SURGE VALVE FILTER ELEMENT SPRING MISSING. INSTALLED THE SPRING IAW AMM 49-53-06.

Part: ISOLATION VALVE — INOPERATIVE (RIGHT) · airframe 80,997 hrs · 23,559 cycles

RIGHT ISOLATION VALVE INOPERATIVE. REMOVED AND REPLACED THE ISOLATION VALVE. OPS CHECKED NORMAL, NO LEAKS IAW AMM 36-11-04.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 80,997 hrs · 23,559 cycles

MESSAGE FOR THE LT PACK BITE. REMOVED AND REPLACED THE LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECKED NORMAL.

Part: ISOLATION VALVE — FAILED (BLEED AIR SYS) · airframe 80,953 hrs · 23,550 cycles

RIGHT ISOLATION VALVE FAILED. R&R RT ISOLATION VALVE, OPS CHECK NORMAL, NO LEAKS IAW AMM 36-11-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT IDG) · airframe 80,953 hrs · 23,550 cycles

MAINTENANCE MESSAGE FOR RT IDG OUT TEMP. CHECKED SERVICING OF IDG IAW AMM 12-12-03. CHECKED GOOD. CLEARED MAINTENANCE MESSAGE, NO FILTER BYPASS BUTTON POPPED.

Part: RIVET — LOOSE (NR 1 NACELLE) · airframe 80,816 hrs · 23,522 cycles

DURING PRE-FLIGHT, MULTIPLE ENGINE COWL RIVETS LOOSE IN THE NR 1 ENGINE. REMOVED AND REPLACED THE RIVETS IAW SRM 51-40-02-0G-0, AND CMM 71-11-16, FIG 1. LT NOSE COWL RIVETS SMOOTH AND SECURE ACFT RELEASE TO CONTINUE SERVICE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 80,788 hrs · 23,515 cycles

EMERGENCY LIGHT INOPERATIVE AT THE RT EMERGENCY ESCAPE HATCH AND AT SEAT 1J. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-05, OPS CHECKED GOOD.

Part: HANDLE — LOOSE (L4 DOOR) · airframe 80,997 hrs · 23,559 cycles

FOUND THE L4 DOOR OPEN HANDLE LOOSE AND CANNOT OPEN DOOR. SECURED THE DOOR HANDLE MECHANISM IAW AMM 52-11-25-402-012. OPS CHECKED GOOD.

Part: START VALVE — INOPERATIVE (LT ENGINE) · airframe 80,696 hrs · 23,495 cycles

LEFT ENGINE START VALVE DID NOT OPEN R & R THE LT ENGINE START VALVE ASSY IAW AMM 80-11-02. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 80,697 hrs · 23,496 cycles

FWD EQUIPMENT OVERHEAT EICAS MESSAGE AND DISCRETE MESSAGE. COMPLIED WITH EQUIPMENT COOLING OPERATIONAL CHECK IAW AMM 21-58-00. EQUIPMENT COOLING CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL QTY) · airframe 80,673 hrs · 23,488 cycles

STATUS MESSAGE FOR FUEL QTY CHANNEL. COMPLIED WITH FQIS BITE IAW AMM 28-41-00, NO FAULTS, SYS OK FOR SERVICE.

Part: FILTER — NOT REPORTED (RT IDG) · airframe 80,638 hrs · 23,480 cycles

INTERMITTENT RT IDG OUT TEMP. REMOVED AND REPLACED THE RT ENG IDG FILTER ASSY IAWAMM 24-11-02, OPS CHECKED & LEAK CHECKED GOOD IAW AMM 24-11-02.

Part: TRANSMITTER — FAILED (RT ENGINE OIL) · airframe 80,516 hrs · 23,454 cycles

RIGHT ENGINE OIL LEVEL READING OFF SCALE. REMOVED AND REPLACED OIL LEVEL TRANSMITTER IAW AMM 79-31-01/401. OPS AND LEAK CHECKED OK.

Part: SWITCH — FAILED (RT ENG BLEED) · airframe 80,476 hrs · 23,447 cycles

RT ENGINE BLEED AIR SWITCH DOES NOT POP OUT COMPLETELY WHEN TURNED OFF. REMOVED AND REPLACED THE SWITCH IAW SWPM 20-84-14. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD PUMP) · airframe 80,456 hrs · 23,443 cycles

RIGHT PRIMARY HYD PUMP EICAS MESSAGE CAME ON IN FLIGHT. TROUBLESHOT IAW FIM 29-11. ALL OPS CHECKS NORMAL. INSPECTED PRESSURE SWITCH CONNECTOR IAW AMM 29-11-17, CONNECTOR IS CLEAN NO CORROSION PRESENT. ACFT OK FOR SERVICE.

Part: ACCELEROMETER — MALFUNCTIONED (LT ENGINE) · airframe 80,495 hrs · 23,450 cycles

ON CLIMB OUT LT ENG VIBRATION INDICATOR FAN 4.1. INSTALLED ALT ACCELEROMETER IAW AMM 77-31-01. ACCOMPLISHED FAN LUBE IAW AMM 72-31-02. ENG RUN IAW AMM 71-00-00 FAN VIBRATION CHECKED GOOD.

Part: IDG — OVERSERVICED (RIGHT) · airframe 80,399 hrs · 23,434 cycles

ATER LANDING, STATUS MESSAGE FOR RT IDG OUT TEMP. TROUBLESHOT IAW FIM 24-20, FOUND RT IDG OVERSERVICED. CORRECTED IAW AMM 12-13-03.

Part: PRESSURE SWITCH — LEAKING (APU) · airframe 80,390 hrs · 23,432 cycles

APU OIL PRESSURE SWITCH LEAKING. REMOVED AND REPLACED APU OIL PRESSURE SWITCH IAW AMM 49-94-02. RAN APU, NO LEAKS DETECTED.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYS) · airframe 80,349 hrs · 23,424 cycles

APU LOW OIL PRESSURE SWITCH LEAKING. REMOVED & REPLACED THE OIL PRESSURE SWITCH ASSY IAW AMM 49-94-02, OPS & LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,292 hrs · 23,410 cycles

RIGHT SLIDE GROUND LIGHTS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW 33-51-06902-082. OPS CHECKED GOOD.

Part: WIRE — OPEN (EMERGENCY LIGHTS) · airframe 80,292 hrs · 23,410 cycles

PASSENGER CABIN FLOOR EMERGENCY LIGHTING INOPERATIVE AT SEAT ROW 1 LT AND RT. CLEANED AND SECURED EMERGENCY POWER SUPPLY UNIT ELECTRICAL CONNECTOR IAW SWPM 20-60-01 SECURED OPEN CONTACT FOUND AT SEAT 2JL IAW WDM 33-51-16. OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 80,292 hrs · 23,410 cycles

L1 EXTERIOR DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE FUSE ON THE BATTERY PACK M736 AT BS 467 IAW WPM 33-51-25. OP CHECKED GOOD IAW AMM 33-51-07-422-012.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,292 hrs · 23,410 cycles

PASSENGER CABIN DOOR EMERGENCY LIGHT INOPERATIVE AT DOOR 2L, 2R, AND 39JL. TROUBLESHOT, AND REPLACED THE LAMPS. OPS CHECKED GOOD IAW WDM 33-51-12.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 80,292 hrs · 23,410 cycles

PASSENGER CABIN FLOOR EMERGENCY LIGHTING INOPERATIVE AT SEAT ROWS 4 THRU 10 LT AND RT. CLEANED AND SECURED EMERGENCY POWER SUPPLY UNIT NR 1 ELECTRICAL CONNECTOR, SECURED OPEN CONTACT AT SEAT 4, OPS CHECKED GOOD IAW SWPM 20-60-01, AND WDM 33-51-18.

Part: VALVE — MALFUNCTIONED (TRIM AIR) · airframe 80,222 hrs · 23,397 cycles

PER CREW REPORT COCKPIT TRIM AIR VALVE HAS FAILED MULIPLE TIMES AND THEN STARTED WORKING AGAIN ON LAST FEW LEGS. REMOVED AND REPLACED FLT DECK ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-07 OPS CHECKED NORMAL.

Part: RADAR — NO TEST (WX SYS) · airframe 80,142 hrs · 23,382 cycles

LEFT WX RADAR SYSTEM FAILED. LEFT WX RADAR SYSTEM TEST & CARRIED OUT IAW AMM 34-43-00. TEST PASSED, OK FOR SERVICES.

Part: VALVE — NO TEST (RT ENGINE) · airframe 80,155 hrs · 23,385 cycles

ON STARTING THE RT ENGINE SPAR VALVE FAILED OPS CHECK IAW AMM 28-21-02.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 80,082 hrs · 23,370 cycles

RIGHT PIMU MAINTENANCE MESSAGE. TROUBLESHOOTING SHOWS CODE 353-224. PERFORMED FIM 71-01-43. SYSTEM CHECKED NORMAL.

Part: ANTI-ICE VALVE — SLOW (RT NACELLE) · airframe 80,082 hrs · 23,370 cycles

RIGHT ENGINE NACELLE ANTI-ICE VALVE IS VERY SLOW TO INDICATE OPEN IN COLD WEATHER. REMOVED AND REPLACED THE ANTI-ICE VALVE. OPS CHECKED GOOD IAW AMM 30-21-03.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 80,082 hrs · 23,370 cycles

RIGHT PIMU MAINTENANCE MESSAGE. TROUBLESHOOTING SHOWS CODE 353-224. PERFORMED FIM 71-01-43 & SYSTEM OPS NORMAL.

Part: EEC — FAILED (LT ENGINE) · airframe 80,045 hrs · 23,361 cycles

STATUS MESSAGE EICAS DISAGREE DISPLAYED. DURING TROUBLESHOOTING, FOUND CODE 514 N1 LEFT, CODE 516 N2 LEFT, LT ENGINE HIGH OIL TEMP, SUSPECT LT ENGINE EEC FAILED. REMOVED & REPLACED THE EEC.

Part: INDICATOR — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,056 hrs · 23,365 cycles

RIGHT ENGINE BLEED AIR SWITCH, MECHANICAL FLOW BAR INDICATOR STICKS IN THE ON POSITION. VERIFIED THE RT ENGINE BLEED SWITCH OPS NORMAL IAW AMM 36-11-26.

Part: LIGHT — INOPERATIVE (ANTI ICE VALVE) · airframe 80,008 hrs · 23,354 cycles

RT ENGINE ANTI-ICE VALVE LIGHT INOPERATIVE. REMOVED AND REPLACED THE ANTI-ICE LIGHT ASSY. IAW AMM 33-11-00. OPS CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE SYS) · airframe 79,948 hrs · 23,342 cycles

RT ENG ANTI-ICE VALVE ILLUMINATED AFTER ENGINE START WITH SWITCH ON. OPERATED SEVERAL TIMES DURING FLIGHT OPS, CHECKED OK. PERFORMED GROUND TEST IAW AMM 30-21-03. CHECKED GOOD.

Part: DUCT — LEAKING (LT MLG WW) · airframe 79,924 hrs · 23,337 cycles

AIR LEAK IN LEFT MLG WW. FOUND DUCT BELOW CENTERT ISOLATION VALVE CRACKED. REMOVED AND REPLACED THE DUCT ASSY IAW AMM 36-11-01. NO LEAKS NOTED.

Part: VALVE — FAILED (RT A/C PACK) · airframe 79,879 hrs · 23,319 cycles

MTC MESSAGE RT PACK BITE. CONTROLLER FAULTED RT PACK LOW CONTROL VALVE, REPLACED LOW LIMIT VALVE REF AMM 21-51-11, OPS CHECK OK.

Part: CIRCUIT CARD — INOPERATIVE (SPAR VALVE) · airframe 79,881 hrs · 23,320 cycles

LEFT SPAR VALVE FAILED ON ENGINE SHUT DOWN. TROUBLESHOT IAW FIM 28-22 14, R & R THE LT SPAR VALVE LIGHT DIODE, FUSE CARD IAW AMM 33-16-02. OPS CHECKED OK.

Part: VALVE — MALFUNCTIONED (ANTI ICE SYS) · airframe 79,843 hrs · 23,310 cycles

EICAS MESSAGE FOR RT ENGINE ANTI-ICE, QRH PROCEDURE PERFORMED. CONFIRMED VALVE OPERATION IAW AMM 30-21-03. REMOVED AND REPLACED THE RT ENGINE TAI VALVE IAW AMM 30-21-03. LEAK AND OPS CHECKED, NDICATIONS NORMAL.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYS) · airframe 79,753 hrs · 23,290 cycles

ON POST FLIGHT WALK AROUND, FOUND OIL DRIPPING FROM APU COWLING. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH IAW AMM 49-94-02. NO LEAKS NOTED.

Part: CONTROLLER — FAILED (LT A/C PACK) · airframe 79,744 hrs · 23,287 cycles

LEFT PACK TEMP CONTROL FAULT. R & R THE A/C PACK CONTROLLER. OPS CHECKED GOOD IAW AMM 21-51-14.

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK) · airframe 79,744 hrs · 23,287 cycles

RIGHT PACK TEMP CONTROL FAULT. REMOVED AND REPLACED THE RIGHT A/C PACK CONTROLLER ASSY IAW AMM 21-51-14. OPS CHECKED NORMAL.

Part: VALVE — FAILED (LT A/C PACK) · airframe 79,708 hrs · 23,280 cycles

ECS MESSAGE LT PACK. REMOVED AND REPLACED LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS & BITE CHECKED GOOD .

Part: A/C PACK — FAULTED (LEFT) · airframe 79,685 hrs · 23,274 cycles

LEFT PACK TEMP EICAS MESSAGE. PERFORMED BITE ON LT PACK CONTROLLER IAW FIM 21-51 FT 803. FAULTED LT PACK TEMP CONTROL VALVE. RESET LT PACK CONTROLLER PERFORMED BITE PREOCEDURE A SECOND TIME. NO CURRENT FAULTS NOTED. NO EICAS MSGE PRESENT. ACFT OK FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,635 hrs · 23,265 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS, CONNECTED THE CONNECTOR FOR SEATS 4-9CA, REMOVED AND REPLACED THE INVERTER, REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHT ASSY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,635 hrs · 23,265 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED THE LAMPS, CLEANED AND REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

Part: MODULE — FAILED (AIR SUPPLY) · airframe 79,635 hrs · 23,265 cycles

UNABLE TO CLEAR AIR SUPPLY BITE MODULE FAULTS. REMOVED AND REPLACED AIR SUPPLY BITE MODULE.

Part: CIRCUIT BREAKER — BROKEN (FUEL JETTISON) · airframe 79,635 hrs · 23,265 cycles

RIGHT FUEL JETTISON PUMP CIRCUIT BREAKER (C376) ON P37 BROKEN. REMOVED AN REPLACED THE CIRCUIT BREAKER.

Part: RELAY — FAILED (BOOST PUMP) · airframe 79,635 hrs · 23,265 cycles

RIGHT FWD BOOST PUMP PRESS LIGHT INDICATION ON PUSH BUTTON SWITCH FAILED TO COME ON WITH GFI TRIPPED. REMOVED AND REPLACED TIME DELAY RELAY (K-5) ON FUEL CONTROL PANEL FOR RIGHT FWD BOOST PUMP PRESS LIGHT INDICATION.

Part: PANEL — BROKEN (MLG DOOR) · airframe 79,580 hrs · 23,254 cycles

ON POST FLIGHT INSPECTION FOUND PANEL 651VB BROKEN, MLG STRUT DOOR BOLT MISSING & MLG TRUNNION DOOR & LEADING EDGE DAMAGED. PERFORMED TEMP REPAIRS PER EO 6757A120 & EO 6752A038. REMOVED STRUT DOOR PER CDL 32-12-01.

Part: PROCESSOR — FAULTED (FUEL QTY) · airframe 79,468 hrs · 23,231 cycles

AFTER TAKE OFF FUEL QTY WAS ERRATIC THEN SETTLED AFTER LEVEL OUT. TROUBLESHOT IAW FIM. FAULTED PROCESSOR REMOVED AND REPLACED IAW AMM 28-41-08 OPS CHECK AND BITE CHECKED NORMAL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 79,404 hrs · 23,216 cycles

EMERGENCY LIGHT COVER AT SEAT 38J IS MISSING. REPLACED THE EMERGENCY LIGHT COVERS IAW MM 25-27-09.

Part: EEC — MALFUNCTIONED (APU) · airframe 79,404 hrs · 23,216 cycles

APU SHUTDOWN. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. OPS CHECKED NORMAL.

Part: BULB — INOPERATIVE (AC BAY) · airframe 79,292 hrs · 23,191 cycles

RIGHT PACK COMPRESSOR OUTLET TEMP INDICATION BLANK. R & R RT PACK COMPRESSOR OUTLET TEMP BULB. OPS CHECK GOOD IAW AMM 21-52-01.

Part: APU — LEAKING (APU BAY) · airframe 79,149 hrs · 23,158 cycles

APU OIL QTY MESSAGE ON STATUS PAGE. OIL FOUND IN TAIL PIPE. TRANSFERRED TO DMI; MDDR 69791 IAW MEL 49-11-01B, CAT B. REMOVED AND REPLACED APU IAW WORK CARD T1071 AMM 49-11-01.

Part: ENGINE — STALLED (LEFT) · airframe 79,126 hrs · 23,153 cycles

LEFT ENGINE COMPRESSOR STALLS WITH HEAVY YAW APPROX 13000-14000. REDUCED THRUST TO IDLE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE ENGINE, OPS CHECKED OK. ACFT RELEASED FOR SERVICE.

Part: BUSHING — WORN (L4 DOOR) · airframe 78,978 hrs · 23,119 cycles

L4 DOOR OPENING HANDLE LOOSE WHEN CLOSED. REPLACED THE HANDLE WORN BUSHING IAW AMM 52-11-25. NO RIGGING WAS REQUIRED. DOOR HANDLE OPERATED NORMAL.

Part: MASK — DAMAGED (PBE) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN R4 PBE DAMAGED. REMOVED AND REPLACED PBE MASK IAW AMM 25-60-00.

Part: LIFE RAFT — LOW PRESSURE (ROW 20) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN ROW 20 LIFE RAFT PRESSURE GAUGE READS LOW. REMOVED THE RAFT ASSY. ROUTED TO VENDER FOR SERVICE IAW AMM 25-05-03. REINSTALLED RAFT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN EMERGENCY LIGHT ROW 5 LT AISLE CEILING INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 78,978 hrs · 23,119 cycles

RIGHT ROW 40 FLOOR EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR ROW 40. CLEANED AND RESET CONNECTOR. EMERGENCY LIGHTS OPS OK. IAW SSM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN ROW 9 RIGHT FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-53-00. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN ROW 31 FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-00. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN LEFT EMERGENCY LIGHT BETWEEN ROW 39 AND AFT GALLEY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHTS IAW AMM 33-53-00 OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,978 hrs · 23,119 cycles

MAIN CABIN ROW 32 FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-00, OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL QTY) · airframe 78,958 hrs · 23,114 cycles

AFTER LANDING STATUS MESSAGE FUEL QTY CHANNEL. FQIS PROCESSOR BITE TEST CARRIED OUT IAW AMM 28-41-00, ALL TESTS PASSED, MESSAGE ERASED.

Part: SEAL — LEAKING (RT A/C PACK) · airframe 78,907 hrs · 23,103 cycles

RIGHT PACK BAY AIR LEAK ABOVE RE-HEATER CONTROLLER. REPLACED THE SEALS. LEAK CHECKED OK IAW MM 21-51-00.

Part: FILTER — DAMAGED (RT ENGINE IDG) · airframe 78,868 hrs · 23,093 cycles

ON POST FLIGHT WALK AROUND, FOUND RT ENG IDG FILTER DP BUTTOM POPPED. REPLACED THE FILTER IAW MM 24-11-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED DUCT) · airframe 78,841 hrs · 23,086 cycles

RIGHT BLEED DUCT LEAKING. PERFORMED OPS CHECK OF AIR SUPPLY SYSTEM. SYSTEM CHECKED NORMAL IAW MM 36-21-00.

Part: FAN — FAILED (FWD EQUIPMENT) · airframe 78,836 hrs · 23,084 cycles

FWD EQUIP OVERHEAT MESSAGE. REMOVED AND REPLACED THE FWD EQUIPMENT SUPPLY FAN IAW AMM 21-58-06, OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E OVERHEAT) · airframe 78,821 hrs · 23,081 cycles

EQUIPMENT OVERHEAT MESSAGE. ACCOMPLISHED QRH SELECRTOR TO STBY FOR 5 MIN THEN OVRD FOR 30 MIN. SELECTOR BACK TO AUTO . OVERHEAT LIGHT EXTINGUISHED . CONT FLIGHT NORMAL. PERFORMED EQUIPMENT COOLING TEST IAW AMM 21-58-00. NO FAULTS FOUND AT THIS STATION.

Part: ACTUATOR — FAILED (FUEL SHUTOFF) · airframe 88,495 hrs · 16,815 cycles

LT SPAR VALVE NO INDICATION ON ENGINE START. REMOVED AND REPLACED FUEL SHUTOFF ACTUATOR IAW AMM 28-22-11.

Part: EEC — FAULTY (LT ENGINE) · airframe 78,618 hrs · 23,033 cycles

STATUS MESSAGE LT ENGINE, ELECTRONIC ENGINE CONTROL T/S IAW FIM 71-00, TASK A17. R & R LT ENGINE, ENGINE CONTROL UNIT IAW AMM 73-21-13, RAN ENGINES. OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,618 hrs · 23,033 cycles

STATUS MSG, LT ENGINE, ELECTRONIC ENGINE CONTROL, C1 CLEARED MSG IAW AMM 31-35-00, TEST OF THE LT PIMU IAW FIM 71-01, TR 811, FAULT CLEARED. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,603 hrs · 23,030 cycles

LEFT ENGINE ELECTRONIC ENGINE CONTROL C1, PERFORMED ELECTRONIC ENGINE CONTROL LT PIMU BITE, CK 350-18A LATCHED RESET CLEARED, CHECKED CONNECTOR PLUG CONNECTORS ON ENGINE. ELECTRONIC ENGINE CONTROL UNIT, CHECKED CONNECTOR PLUG AT PYLON CONNECTOR, NO DEFECTS FIM 71-01, FT810, MM 71-00-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,580 hrs · 23,025 cycles

STATUS MESSAGE, LT ENGINE ELECTRONIC ENGINE CONTROL C1. CLEARED MESSAGE IAW AMM 31-35-00, PERFORMED TEST OF LT PIMU, DATA MODE DISAGREE, FOLLOWED FIM 71-01 F, TREE 811, CLEARED FAULTS SYS, CKS NORMAL.

Part: CONNECTOR — UNSECURE (RT IGNITOR) · airframe 78,506 hrs · 23,009 cycles

RIGHT ENG IGNITOR 1 STATUS MSG. PLACED ON MEL 74-00-01B, MDDR 67109. SECURED CONNECTOR SOCKETS AT AW0325 CONNECTION SYS TEST IAW AMM CH 74-00-00. RT ENG IGNITOR OPERATES NORMAL MDDR 97109 CLOSED.

Part: EXCITER — MALFUNCTIONED (RT ENGINE) · airframe 78,506 hrs · 23,009 cycles

RIGHT ENG IGNITER 1 R & R RT ECU AMM 73-21-13 & RT ENG NR 1 IGNITER EXCITER IAW AMM 74-11-01. OPERATIONS CHECKED NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,473 hrs · 23,002 cycles

RIGHT ENG IGNITOR 1 STATUS MSG. MSG CLEARED USING MCDP EICAS ERASE PROCEDURES IAW AMM 31-41-02. SYS CHECKED OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EXCITER BOX) · airframe 78,432 hrs · 22,995 cycles

RIGHT ENG IGNITER 1 STATUS MSG. PLACED DEFERRAL 74-00-01B MDDR 66953. FOUND CONNECTOR ON EXCITER BOX LOOSE, TIGHTENED SAME OPS CHECKS GOOD THIS CLEARS MDDR 66953 AMM 74-11-01.

Part: CONTROLLER — DEFECTIVE (BLEED AIR SYS) · airframe 78,432 hrs · 22,995 cycles

RIGHT ENG HPSOV STATUS MSG. PLACED ON DDG 36-11-02-02 & MDDR 66954. RT HP CONTROLLER REPLACED ON LP 764074 , M3. REACTIVATED HP VALVE, SYSTEM TESTED NORMAL DURING ENG RUN PER MM CH 36-11-07. MDDR CLEARED.

Part: ENGINE — LEAKING (NR 2) · airframe 78,425 hrs · 22,994 cycles

DURING POWER RUN POST WALK, FOUND NR 2 ENG WITH OIL LEAK FROM AFT BEARING LINE. R & R RT ENG ASSEMBLY IAW WO 15415. LEAK & OPERATIONS CHECKED GOOD.

Part: FITTING — DISCONNECTED (BLEED AIR SYS) · airframe 78,425 hrs · 22,994 cycles

RT STRUT DUCT LEAK EICAS MSG. FOUND PRE COOLER EXHAUST FITTING DISCONNECTED BETWEEN PRE COOLER & PRSOV. REPOSITIONED FLANGE & SEAL ASSEMBLY IAW AMM 36-11-15, RAN HIGH POWER IAW AMM 71-00-00, ALL OPERATIONS CHECKED GOOD.

Part: ACM — FAULTY (AC BAY) · airframe 78,421 hrs · 22,993 cycles

LEFT PACK INOPERATIVE LIGHT. REPLACED LT PACK ACM IAW AMM 21-51-03. OPERATIONS & LEAK CHECKS GOOD.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 78,421 hrs · 22,993 cycles

RIGHT ENG BLEED OFF & RT PACK OFF, EICAS MSG INTERMITTENT DURING CLIMB. RAN BITE ON PNEUMATIC CONTROLLER FAULTED FAN AIR MOD VLV. INSPECTED VLV, CLEANED CONNECTOR & CYCLED VLV IAW AMM 36-11-16. PERFORMED BITE AGAIN, ALL CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,410 hrs · 22,992 cycles

AT DEPARTURE LT PACK INOPERATIVE LIGHT. FOUND LT PACK OVERTEMP ON BITE BOX. RESET BOX, OPENED PACK BAY DOORS, NO PROBLEMS NOTED, SYS OK IAW AMM 21-51-03.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 78,410 hrs · 22,992 cycles

RIGHT ENG BLEED OVERHEAT ADVISORY MSG AFTER TAKEOFF, CLEARED IAW QRH PROCEDURE. TROUBLE SHOT IAW FIM 36-10 TREE 835, FOUND HPSOV BAD. R & R HPSOV IAW AMM 36-11-07. DRY MOTORED ENG LEAK CHECKS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,398 hrs · 22,991 cycles

RIGHT ENG HPSOV ADVISORY MSG. QRH COMPLETED. COMPLIED WITH FIM 36-10 TREE 832 BITE CHECK ON PNEUMATIC CONTROLLER, NO FAULTS. CLEARED MSG & SYS CHECKED OK.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 78,338 hrs · 22,987 cycles

RIGHT DUCT PRESS FLUCTUATES ON TAKEOFF. R & R NR 2 ENG HPSOV IAW AMM 36-11-07-024-001-001 & AMM 36-11-07-424-016-00. ACCOMPLISHED BLAST FENCE RUN & BLEED OPERATION IS NORMAL IAW AMM 71-00-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,378 hrs · 22,988 cycles

RIGHT ENG HPSOV STATUS MSG DISPLAY. COMPLIED WITH FIM 36-10 TREE 832 BITE CHECK. PNEUMATIC CONTROLLER NO FAULT CLEARED HPSOV & STATUS MSG USING AUTO ERASE FUNCTION SYS CHECK OK AT THIS TIME.

Part: DUCT — DAMAGED (APU) · airframe 78,344 hrs · 22,978 cycles

APU RUBBER DUCT FROM ENG, OUT TO SURGE VLV, HAS A HOLE. REMOVED & INSTALLED AIR SURGE DUCT, PN 3884292-2, IAW AMM 49-53-01-404-010. OPERATED APU NO LEAKS NOTED IAW AMM 49-00-00.

Part: COVER — DAMAGED (CABIN) · airframe 78,344 hrs · 22,978 cycles

MAIN CABIN LT ROW 19 FLOOR EMER LIGHTS TRACK COVER DAMAGED. REPLACED EMER LIGHT TRACK COVER ON LT ROW 19 IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL AT THIS TIME.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 78,344 hrs · 22,978 cycles

LEFT ENG 350 27-NO 28VDC DETECTED. R & R RELAY XLD4N009 K1036. OPERATIONS CHECKED OK IAW 31-41-00.

Part: COVER — DAMAGED (CABIN) · airframe 78,344 hrs · 22,978 cycles

MAIN CABIN RT 21 FLOOR EMER LIGHTS TRACK COVER, TAPED IN PLACE. REPLACED EMER LIGHT TRACK COVER ON RT ROW 21 IAW AMM 33-53-00. OPERATIONS CHECK NORMAL AT THIS TIME.

Part: BEARING — DEFECTIVE (NR 2 ENGINE) · airframe 78,344 hrs · 22,978 cycles

NUMBER 2 ENG PNEUMATIC DUCT ATTACHMENT ROD, AT APPROX 10 O'CLOCK POSITION, HAS ONE ROD END BAD BEARING, ATTACHED TO ENG FLANGE. R & R THE ROD END BEARING ON THE UPPER SUPPORT LINK. FOR THE PNEUMATIC DUCT IAW AMM 80-11-05-004-016-H00 & 80-11-05-404-006-H00.

Part: COMPRESSOR BLADE — NICKED (NR 2 ENGINE) · airframe 78,344 hrs · 22,978 cycles

NUMBER 2 ENG HAS VARIOUS OF FAN BLADES NEED DRESSING UP. BLENDED OUT SMALL NICKS AT NR 2 ENG FAN BLADES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLUORESCENT PENETRANT INSPECTION. FOUND NICKS REMOVED, NO CRACKS IAW AMM 70-11-06 PB 201.

Part: COMPRESSOR BLADE — NICKED (NR 1 ENGINE) · airframe 78,344 hrs · 22,978 cycles

NUMBER 1 ENG HAS SOME FAN COMPRESSOR BLADES THAT NEED DRESSING UP. BLENDED OUT ALL NICKS AT NR 1 ENG FAN BLADES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLUORESCENT & PENETRANT INSPECTION. FOUND NICKS REMOVED & NO CRACKS FOUND IAW AMM 70-11-06 PB 201.

Part: ECU — MALFUNCTIONED (NR 1 ENGINE) · airframe 78,344 hrs · 22,975 cycles

LEFT ENG 353 24-B LOW PRESSURE TURBINE CASING T/M W/A FAIL. R & R NR 1 ENG ECU IAW MM 73-21-15-404-068-HOO. PERFORMED NR 3 GND TEST OK 71-00-00.

Part: ECU — FAILED (NR 1 ENGINE) · airframe 78,344 hrs · 22,978 cycles

LEFT ENG 353 21-B HPTC T/M W/A FAIL. R & R NR 1 ENG ECU IAW AMM 73-21-15. PERFORMED TEST 3 GND TEST OK AMM 71-00-00.

Part: INLET — CRACKED (NR 2 COWLING) · airframe 78,344 hrs · 22,978 cycles

NUMBER 2 ENG PRE-COOLER RAM INLET, SQUARE ENTRANCE ON INBD COWL SIDE HAS CRACK. REMOVED CRACKED PRE-COOLER RAM INLET SQUARE ENTRANCE ON INBD REVERSER IAW SRM 51-40-02-06. PREPARED, CLEANED & REPAIR AREA'S WITH CRACKS IAW SRM 51-70-07-00-0 & 250 DEG F CURE PERMANENT HOT BOND REPAIR ACCOMPLISHED. LOCATED & INSTALLED REPAIRED PRE-COOLER RAM INLET, SQUARE ENTRANCE MASKED & SEALED IAW SRM 51-40-02-06 & 51-20-05-00-0.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 78,344 hrs · 22,978 cycles

NUMBER 2 ENG PRE-COOLER RAM AIR DUCT ON COWLING HAS A CRACK. R & R AIR SUPPLY DUCT IAW AMM 36-11-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,330 hrs · 22,976 cycles

STATUS MSG RT ENG HPSOV. PERFORMED HPSOV TEST ON AIR SUPPLY BITE MODULE IAW AMM 36-11-07-714-031-001, RT ENG HPSOV NO FAULTS, CLEARED MSG. ACFT CLEARED TO CONTINUE NORMAL OPERATIONS.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,220 hrs · 22,952 cycles

LEFT ENG FIRE LOOP 1 STATUS MSG. NO ACTIVE MSGS FOUND FIRE TEST CARRIED OUT IAW AMM 26-11-00. ALL TEST SATISFY.

Part: LENS — MISSING (CABIN) · airframe 78,215 hrs · 22,950 cycles

EMERGENCY LT LENS MISSING AT RT WING EMER DOOR, BELOW DOOR. LOCATED & INSTALLED MISSING LENS IAW AMM 33-57-00.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,220 hrs · 22,952 cycles

APU DID NOT LIGHT AFTER TOUCH DOWN. TROUBLE SHOT APU IAW AMM 49-61-05. PERFORMED APU ECU BITE TEST. NOTED FAULT, ABORTED START, STARTED APU SEVERAL TIMES ON GND. OPERATIONS CHECKED GOOD.

Part: FIRE LOOP — FAULTY (LT ENGINE) · airframe 78,191 hrs · 22,945 cycles

LEFT ENG FIRE LOOP 2 EICAS MSG. TRANSFERRED TO MDDR 66104 IAW DDG 26-11-01-01 CAT C. ACFT LIMITED TO 120 MIN ETOPS. R & R LT ENG LOWER AFT FIRE LOOP IAW AM 26-11-02. OPERATIONS CHECKED GOOD, CLEARED MDDR 66104. REMOVED PLACARD & NOTIFIED MCC.

Part: FIRE LOOP — FAULTY (LT ENGINE) · airframe 77,862 hrs · 22,869 cycles

STATUS MSG LT ENG FIRE LP1. TRANSFERRED TO MEL 26-11-01-01 23 MAR, LP 727420, ITEM M3. R & R ENG 1 UPPER AFT DETECTION LOOP IAW MM 26-11-02, TEST 26-11-00 OK & CLEARS MDDR.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 77,845 hrs · 22,865 cycles

LEFT ENG FIRE LP 1 STATUS, FWD TO MDDR 65184 IAW MEL 26-11-01-01-CAT C DUE 31 MAR 16, PLACARD INSTALLED. PERFORMED ENG FIRE LOOP TEST IAW AMM 26-11-00. ALL CHS NORMAL, PLACARD REMOVED. MCC NOTIFIED & CLEARED MDDR 65184.

Part: SEAL — LEAKING (CABIN WINDOW) · airframe 77,798 hrs · 22,853 cycles

SEAT LOCATED 2L WINDOW SEAL LEAKING. R & R WINDOW SEAL LOCATED AT 2L SEAT POSITION IAW AMM 56-21-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,798 hrs · 22,853 cycles

MAIN DECK AFT CEILING EMER LIGHT INOPERATIVE. RELAMPED MAIN DECK AFT CEILING EMER LIGHT IAW AMM 33-51-04. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,798 hrs · 22,853 cycles

RIGHT EXTERIOR EMER LIGHT FWD OF AFT CARGO DOOR INOPERATIVE. RELAMPED RT EXTERIOR EMER LIGHT FWD OF AFT RT CARGO DOOR IAW MM 33-51-16. OPERATIONS CHECKED OK.

Part: DUCT — DAMAGED (APU BAY) · airframe 77,798 hrs · 22,853 cycles

VENTILATION DUCT OF APU DAMAGED. R & R VENTILATION DUCT COOLING AT APU COMPARTMENT LT SIDE IAW & MM 49-51-01.

Part: TRANSMITTER — LEAKING (APU) · airframe 77,798 hrs · 22,853 cycles

SWITCH 8TJ99GGE1 WITH OIL LEAK IN GEAR BOX OF APU. R & R OIL TRANSMITTER IAW 49-94-04 & SERVICED APU OIL. ACCOMPLISHED OPERATIONS CHECK & LEAK CHECK NORMAL, NO LEAKS. R & R CONNECTOR IAW AMM 49-94-03 & 49-94-04.

Part: SEAL — DEFECTIVE (COCKPIT WINDOW) · airframe 77,798 hrs · 22,853 cycles

BAD SEAL ON NR 2 LT MAIN WINDOW, CAPTAINS SIDE MAKING NOISE. R & R NR 2 WINDOW LT PRESS SEAL IAW AMM 56-11-11.

Part: WARNING SYSTEM — MALFUNCTIONED (FUEL SYSTEM) · airframe 77,618 hrs · 22,814 cycles

FORWARD RT FUEL PUMP, WHEN TURNED OFF, NO PRESS LIGHT & NO EICAS MSG. CYCLED FWD RT FUEL PUMP SWITCH. OPERATIONS CHECK SATISFACTORY, UNABLE TO FAULT IAW AMM 28-22-00.

Part: BOLT — MISSING (AC BAY) · airframe 77,544 hrs · 22,797 cycles

AFT EQUIP COOLING 2 INOPERATIVE. MEL 21-58-05 CAT C DUE 25 FEB, PLACARD INSTALLED. INSTALLED & SECURED BOLT IAW SMP 20-11-00. PERFORMED AFT EQUIP COOLING FAN & PERFORMED AFT EQUIP COOLING FAN TEST IAW AMM 21-58-41, OPERATIONS OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 77,543 hrs · 22,796 cycles

FLOOR EMER LIGHTING HAS A SPOT NOT WORKING. FOUND LOOSE CONNECTION AT ROW 16F. CONNECTED WIRE, OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,399 hrs · 22,769 cycles

VARIOUS EMER FLOOR LIGHTS INOPERATIVE. R & R LAMPS AT R40 & R8, R13, L26, L16, L13. OPERATIONS CHECKED NORMAL IAW AMM 33-51-10 & PN 3071BPEGPL 6 EA.

Part: BULB — DEFECTIVE (AC BAY) · airframe 77,375 hrs · 22,765 cycles

DUE TO REPORTS OF LT AC PACK TRIP OFF, FOUND LT PACK COMPRESSOR OUTLET, TEMP BULB FAULTING ON PACK CONTROLLER. TROUBLE SHOT IAW AMM 21-51-14. FOUND LT COMPRESSOR OUTLET TEMP BULB BAD. REPLACED SAME IAW AMM 21-51-06. OPERATIONS & LEAK CHECKED GOOD.

Part: CONNECTOR — DIRTY (WEATHER RADAR) · airframe 77,291 hrs · 22,745 cycles

WEATHER SYS LT RADAR INDICATED, WXR FAIL. REMOVED THE LT WX RADAR TRANSCEIVER, CLEANED CONNECTORS. PERFORMED OPERATIONS CHECK, SYS OK IAW AMM 34-43-00 501.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,276 hrs · 22,742 cycles

ON DEPT PACK TEMP MSG. PERFORMED QRH EICAS PROCEDURE. PERFORMED BITE ON LT PACK CONTROLLER, FAULTED COMPRESSOR SENSOR. COMPLETED RESET & VERIFICATION ALL CHECKED GOOD IAW AMM 21-61-00.

Part: SHUTOFF VALVE — LEAKING (BLEED AIR SYS) · airframe 77,225 hrs · 22,731 cycles

ON WALK AROUND FOUND RT ENG PRSOV LEAKING AIR FROM VLV DIAPHRAGM HOUSING. R & R RT ENG PRSOV. LEAK CHECK OK IAW AMM 36-11-02. ENG RUN OPERATIONS GOOD IAW AMM 72-00-00.

Part: WIRE — BROKEN (BOOST PUMP) · airframe 77,098 hrs · 22,702 cycles

ON PUSHBACK & LT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. PERFORMED TROUBLESHOOTING WDM 28-22-12, FOUND A BROKEN WIRE W176-90H-24 AT TERMINAL BLOCK TB218 YA5. REPAIRED WIRE & REPLACED TD RELAY K10693 AS PRECAUTION. OPERATED LT CENTER BOOST PUMP IAW MM 28-22-00. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,064 hrs · 22,690 cycles

MULTIPLE EMER LIGHTS INOPERATIVE AT FLOOR & CEILING IN ZONES C & D. REPLACED 2 LENSES & LIGHT ASSEMBLIES JUST FWD & AFT OF SEAT 36CA FLOOR IAW AMM 33-51-06. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,066 hrs · 22,690 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED R2 DOOR EXTERIOR EMER LIGHT IAW AMM 33-51-06. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

ENG 2 PRSOV FAILED HEALTH CHECK. R & R ENG 2 PRSOV. LEAK & OPERATIONS CHECK GOOD IAW AMM 36-11-09.

Part: GASKET — LEAKING (OIL COOLER) · airframe 77,066 hrs · 22,690 cycles

ENG 2 HAS A FUEL LEAK, LOCATED BETWEEN MAIN FUEL PUMP & FUEL & OIL HEAT EXCHANGER. R & R GASKET ON ENG 2 IAW AMM 79-21-01. OPERATIONS CHECKED GOOD. NO LEAKS NOTED AT THIS TIME.

Part: LINER — DAMAGED (OVERWING EXIT) · airframe 77,066 hrs · 22,690 cycles

RIGHT FWD OVERWING EXIT DOOR HAS DAMAGE TO DOOR LINER COVERING. CLEANED AREA, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

Part: PRECOOLER — CRACKED (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

ENG 1 PRECOOLER HAS A CRACK ON THE LOWER FWD OTBD CORNER. R & R NR 1 ENG PRECOOLER. OPERATIONS LEAK CHECKED NORMAL IAW MM 36-11-15.

Part: VALVE — NO TEST (NR 1 ENGINE) · airframe 77,066 hrs · 22,690 cycles

NUMBER 1 & ENG PRSOV FAILS HEALTH CHECK. R & R NR 1 ENG PRSOV, OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 36-11-09.

Part: SEAL — DAMAGED (AC BAY) · airframe 77,066 hrs · 22,690 cycles

LEFT ACM TURBINE INLET COUPLING LEAKING AIR. R & R LT ACM TURBINE INLET COUPLING SEALS IAW AMM 21-51-03. LEAK & OPERATIONS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

ENG 2 PART 3 OF EO6736A005 STEP 6 FAILED & PRV DID NOT CLOSE WEN BLEED SWITCH WAS TURNED TO OFF. R & R PRV CONTROLLER. OPERATIONS & LEAK CHECKED GOOD. REF AMM 36-11-19.

Part: BONDING WIRE — FRAYED (RT WING) · airframe 77,066 hrs · 22,690 cycles

RIGHT WING THERMAL WING ANTI-ICE VLV AT TOP OF PYLON, HAS FRAYED BONDING WIRE. REPLACED RT WING THERMAL WING ANTI-ICE VLV BONDING WIRE IAW SWPM 20-20-10.

Part: PRESSURE SWITCH — CORRODED (RT ENGINE) · airframe 77,066 hrs · 22,690 cycles

RIGHT ENG INLET, TAI PRESS SWITCH CONNECTOR IS NOT CONNECTED. PLUG & SWITCH SHOW SIGNS OF CORROSION. CLEANED CONNECTOR IAW SWPM 20-60-01. R & R TAI PRESS SWITCH IAW AMM 30-21-01. OPERATIONS CHECK ACCOMPLISHED ON WC A-30-003-02-2.

Part: SPRING — DEFECTIVE (EVAC SLIDE) · airframe 77,066 hrs · 22,690 cycles

R1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R R1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM GAS SPRING IAW AMM 25-66-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,066 hrs · 22,690 cycles

CABIN FLOOR EMER LIGHTS AT RT SIDE 31, 32 & 40, AFT & LAST LIGHT ON LT SIDE ARE INOPERATIVE. TRACK LIGHTING IS REPLACED IAW AMM 33-51-10. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

NUMBER 2 HP CONTROLLER FAILED HEALTH CHECK. R & R NR 2 HP CONTROLLER IAW AMM 36-11-08.

Part: GROUND WIRE — DISCONNECTED (AC BAY) · airframe 77,066 hrs · 22,690 cycles

LEFT PACK RAM AIR DOOR ACTUATOR GND DISCONNECTED. CONNECTED LT PACK RAM AIR EXHAUST ACTUATOR BONDING JUMPER IAW AMM 21-53-04. RESISTANCE CHECKED GOOD.

Part: MOUNT — BROKEN (NR 1 ENGINE) · airframe 77,066 hrs · 22,690 cycles

CORE MODULE, VAR STATOR VANE LEVER ASSEMBLY AFT MODULATING STUD ON ENG 1, INBD SIDE IS BROKEN. R & R CORE MODULE VAR STATOR VANE LEVER AFT MOUNTING STUD ON ENG 1 IAW AMM 72-36-00.

Part: SPRING — DEFECTIVE (EVAC SLIDE) · airframe 77,066 hrs · 22,690 cycles

L1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R L2 DOOR ESCAPE SLIDE GAS SPRING IAW AMM 25-66-03.

Part: WIRE HARNESS — LOOSE (CABIN) · airframe 77,066 hrs · 22,690 cycles

WIRE BUNDLE AT RT STATION 396 - 412 IS LOOSE. EMER TRACK LIGHTING. SECURED WIRE HARNESS IAW SWPM 20-10-11.

Part: COVER — UNKNOWN (CABIN) · airframe 77,066 hrs · 22,690 cycles

REPLACE EMER LIGHT TRACK COVERS AS REQUIRED WITH NEW. R & R EMER LIGHT TRACK COVERS IAW AMM 33-51-10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 77,066 hrs · 22,690 cycles

LEFT SIDE FLOOR & AISLE EMER LIGHTS INOPERATIVE A ZONE. TROUBLE SHOT RT SIDE EMER FLOOR LIGHTS ZONE A IAW WDM 33-51-16, BATTERY M730 FOUND UNSERVICEABLE. REPLACED BATTERY & OPERATIONS CHECKED IAW AMM 33-51-07.

Part: CLAMP — DEFECTIVE (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

LEFT WW APU PNEUMATIC DUCT SUPPORT CLAMP JUST DOWNSTREAM OF CTR ISOLATION VLV HAS AIR LEAKING FROM UNDERNEATH. R & R CLAMP DOWNSTREAM OF CTR ISOLATION VLV IAW AMM 36-11-01. NO DEFECTS NOTED & LEAK CHECKED GOOD.

Part: SPRING — DEFECTIVE (EVAC SLIDE) · airframe 77,066 hrs · 22,690 cycles

R2 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R R2 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM GAS SPRING IAW AMM 25-66-03.

Part: CONNECTOR — DAMAGED (AC BAY) · airframe 77,066 hrs · 22,690 cycles

CONNECTOR D1338 TO LT PACK COMPRESSOR INLET TEMP BULB TS290 HAS A LOOSE BACK SHELL & POSSIBLE DAMAGED WIRING. REMOVED & INSTALLED NEW CONNECTOR & BACK SHELL AT TEMP BULB TS290 IAW SWPM 20-61-19. OPERATIONS CHECKED GOOD.

Part: GROUND WIRE — FRAYED (AC BAY) · airframe 77,066 hrs · 22,690 cycles

GROUND WIRE FRAYED ON LT HEAT EXCHANGER FWD DUCT. REPLACED BONDING WIRE ON LT HEAT EXCHANGER IAW SWPM 20-20-10. GND BOND CHECKED GOOD.

Part: TRIM PANEL — GOUGED (OVERWING EXIT) · airframe 77,066 hrs · 22,690 cycles

RIGHT AFT OVERWING ESCAPE HATCH WINDOW TRIM & HANDLE LATCH TRIM IS GOUGED. REMOVED DAMAGE, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

Part: CLAMP — UNSECURE (CARGO BAY) · airframe 77,066 hrs · 22,690 cycles

LOWER FWD CARGO BILGE AREA STATION 400, AVIONICS OVERBOARD EXHAUST DUCT HAS CLAMP NOT SECURED AT FLOOR & AROUND DUCT. SECURED STRINGER CLIP IAW SWPM 20-10-12.

Part: SIGN — LOOSE (CABIN) · airframe 77,066 hrs · 22,960 cycles

EXIT SIGN AT 19JL IS LOOSE FROM PANEL, REATTACHED EXIT SIGN ON PANEL AT SEAT 19JL IAW SOPM 20-50-12.

Part: SIGN — CRACKED (CABIN) · airframe 77,066 hrs · 22,690 cycles

OVERHEAD EXIT SIGNS AT AFT & FWD LAVATORY CRACKED & NEEDS PAINT. REPAIRED EXIT SIGNS AT AFT & FWD LOCATIONS IAW AMM 25-00-00-308-166. INSTALLED PLACARDS IAW AMM 20-10-12-404-004, NO PAINT NEEDED.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 77,066 hrs · 22,690 cycles

RIGHT PNEUMATIC ISOLATION VLV INOPERATIVE. TROUBLE SHOT RT PNEUMATIC ISOLATION VLV IAW WDM 36-11-21. CLEANED CONNECTOR IAW SWPM 20-60-01. OPERATIONS CHECKED GOOD IAW AMM 36-11-04.

Part: BYPASS SWITCH — FAILED (LT ENGINE) · airframe 77,066 hrs · 22,690 cycles

LEFT ENG FUEL FILTER BYPASS FAILED STEP B OF TASK CARD 73-306-01-1. R & R , OPERATIONS CHECKED & LEAK CHECKED NR 1 ENG FUEL FILTER BYPASS IAW AMM 73-34-01-424-008 & 73-34-00-715-001-H00 & 71-00-00 001. OPERATIONS CHECKED GOOD, NO LEAKS NOTED AT THIS TIME.