N774AX

Part: A/C PACK — ILLUMINATED · airframe 74,361 hrs · 47,497 cycles

DURING TAXI, C/L IRS DC FAIL EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). CYCLED STANDBY POWER, PER AMM 24-33-00 AND PERF OPS CHECK OF L AND C IRS PER IAW FAULT TREE 34-21. PS CHECK GOOD, A/C REMAINS CAT IIIB. ONE TIME AUTH # 2025-047. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FAULTED (ZONE 100) · airframe 74,334 hrs · 47,480 cycles

DURING TAXI, WITH BOTH ENGINES RUNNING AND CENTER FUEL PUMP SWITCHES ON, CENTER LEFT PUMP PRESS LIGHT ILLUMINATED AND CENTER LT FUEL PUMP EICAS MESSAGE DISPLAYED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED L/H CENTER FUEL PUMP IAW MEL 28-22-2A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARDS INSTALLED. MBCB 11/22/25. L/P 39406-47/1. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (RT A/C PACK) · airframe 74,284 hrs · 47,443 cycles

ON TAXI OUT, RT PACK TEMP EICAS MSG ON. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED SYSTEM IAW MEL C ABX-21-51-1-1. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 74,018 hrs · 47,326 cycles

BULK CARGO DOOR EICAS INTERMITTENT ENTRY DOOR, EMER DOOR & CARGO DOOR DISCREET LIGHTS INTERMITTENT FLASHING. PERFORMED CABIN PRESSURATION IAW B767 AMM 05-51-24. PSEU BITE IAW B767 FIM 32-09 FT 803 AND DOOR WARNING SYSTEM TEST IAW B767 AMM 52-71-00. NO FAULTS NOTED AT THIS TIME. NO MSG PRESENT AT THIS TIME. A/C RETURNED TO SERVICE.

Part: CONTROL PANEL — DAMAGED (ZONE 200) · airframe 73,988 hrs · 47,318 cycles

DURING SERVICE CHECK FOUND UNARMED INDICATION OVERHEAD EMER LIGHTS/CREW OXY PANEL HAS BROKEN KORRY SWITCH R/R OVERHEAD EMERGENCY LIGHTS /CREW OXY PANEL IAW B767 AMM 33-51-08. OPS CHECK GOOD RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (ZONE 100) · airframe 73,973 hrs · 47,314 cycles

DURING TAXI OUT, LEADING EDGE ASYM EICAS MESSAGE,AFTER EXICUTING AFTER START CHECK LIST . AIRCRAFT RETURNED TO BLOCKS (BTB). MTX GROUNDED A/C . C/W OPS CHECK OF THE LE SLATS IAW AMM 27-51-00. FLAPS FAIL LE SLAT ASYM MSG APPEARS . FSEU SHOWING MSG 27-81021. REF FIM FSEU BITE 27-51-FT809 OSEU TARGET CHECK OF S278 SWITCH SHOWS SENSOR READING NEAR WHEN IT SHOULD BE FAR , REMOVED AND REPLACED PROX SWITCH S278 IAW SWPM 20-10-13,20-10-14. OPS CHK FAIL .FURTHER T/S REQ. SEE LP 39227-19/2  PERFORMED CHECK OF THE CIRCUIT BETWEEN THE #3 SLAT OUTBD PROX SENSOR AND THE PSEU CONNECTOR D2166A PINS E10, F10. MH READING GOOD. REMOVED AND REPLACED PSEU IAW AMM 32-09-04, OPS CHKS OK. NO EICAS MSGS S278 PROX SWITCH INDICATE ACCORDINGLY. ALSO REF. WDM 27-88-11.LP 39227-19/2. A/C RETURNED TO SERVICE

Part: WARNING FLAG — ACTIVATED · airframe 73,861 hrs · 47,271 cycles

DURING TAXI OUT, RA FLAG ON THE F/O'S SIDE. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED RIGHT RA IAW MEL 34-33-1-2A-1. ACFT RELEASED TO CAT II OPERATIONAL. PLACARD INSTALLED REF ITEM 2 MBCB 07/27/25. A/C RELEASED TO SERVICE.

Part: MEC — OVERTEMP (ZONE 100) · airframe 73,855 hrs · 47,267 cycles

DURING TAXI OUT "FWD EQP OVHT " ON EICAS , A/C RETURNED TO THE GATE (BTB) MTX GROUNDED A/C. MTX THEN COOLED MEC WITH EXTERNAL AC UNIT , AND PERFORMED OPERATIONAL CHECK OF EQUIPMENT COOLING PER B 767 AMM 21-58-00. OPS CHECK GOOD. A/C WAS HEAT SOAKED DUE TO HIGH TEMPS IN PHX. MTX RETURNED A/C TO SERVICE .

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 73,776 hrs · 47,240 cycles

MAINTENANCE FOUND 3 LH EMERGENCY OVERHEAD LIGHTS IN SUPERNUMERARY AREA INOP. REMOVED AND REPLACED SUPPLY BATTER PACK IAW B767 AMM 33-51-07. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — PILOT ERROR (NONE) · airframe 73,679 hrs · 47,212 cycles

FLIGHT REPORTED THE AIRCRAFT RAN OFF THE RUNWAY AFTER LANDING. THE CREW REPORTED THEY INADVERTENTLY TAXIED INTO THE CONCRETE ISLAND IN FRONT OF INTERSECTION E4 AND BETWEEN D1 AND D2. ONLY THE NOSE GEAR WENT INTO THE ISLAND. IT WAS DETERMINED THERE WAS NO DAMAGE TO THE TAXIWAY, OR AIRPORT LIGHTING, AND A TUG WAS SENT TO PUSH THE AIRCRAFT BACK ONTO THE TAXIWAY.MTX GROUNDED A/C AND MTXPERFORMED IAW AMM 05-51-30 NOSE LANDING GEAR AND FORWARD FUSELAGE INSPECTION. NO DEFECTS FOUND PER PHASE 1A AND 1B.. AND RETURNED AC TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF LIMITS (ZONE 800) · airframe 73,606 hrs · 47,188 cycles

ON TAXI OUT, BULK CARGO DOOR LIGHT ILLUMINATED AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCKS. (BTB). T/S BULK CARGO IND. FOUND PROXIMITY SENSOR GAP OUT OF LIMITS, ADJUSTED PROXY SENSOR GAP PER AMM 52-71-00. OPS CHECKED OK. DI 62576 CLOSED. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: MOUNT — CRACKED (ZONE 400) · airframe 73,382 hrs · 47,105 cycles

DURING A 4 CHECK IN CVG, DURING INSPECTION TASK: ABX-71-001-02-2, FOUND #2 ENG AFT ENGINE MOUNT ATTACHMENT POINT SHEARED ON CONNECTING BOLT. REMOVED AND REPLACED #2 ENG AFT ENGINE MOUNT IAW BOEING 767 AMM 71-21-02 ON FEAM N/R 028. SEE TASK CARD ABX-71-999-03-01 FOR #2 ENG REMOVAL / INTASLL & RII. RETURNED A/C TO SERVICE.

Part: AILERON SYS — MALFUNCTIONED · airframe 73,347 hrs · 47,087 cycles

DURING FLIGHT CONTROL CHECK ON TAXI OUT THE AILERONS WOULD NOT MOVE. AFTER APPROX 5 ATTEMPTS THE AILERONS (YOKE) OPERATED NORMALLY.A/C RETURNED TO THE GATE (BTB) MTX GROUNDED A/C. MTX PERFORMED OPERATIONAL TEST IAW B767 AMM 27-11-00 OPS CHECK GOOD AT THIS TIME. MTX RETURNED A/C TO SERVICE.

Part: LANDING GEAR — FAULTED (ZONE 700) · airframe 73,319 hrs · 47,076 cycles

ON FINAL APPROACH WHEN SELECTED LANDING GEAR HANDLE DOWN THE LANDING GEAR DISAGREE APPEAR FOR MORE THE 45 SECS THEN THE MESSAGE DISAPPEARED. PERFORMED GO AROUND AND LEFT GEAR HANDLE DOWN, AND LANDED WITH NO ISSUES. MTX GROUNDED AC AND PERFORMED FIM. 32-61 FT 812 MEASSAGE CLEARED AND NO FURTHER FAULTS AT THIS TIME . MTX RETURNED AC TO SERVICE .

Part: SPRING — WEAK (AILERONS) · airframe 73,239 hrs · 47,031 cycles

DURING TAXI OUT YOKE WOULD NOT MOVE DURING FLIGHT CONTROL CHECK (AILERON TRIM INOPERATIVE).AC RETURNED TO GATE (BTB) AND MTX GROUNDED ACFT. TROUBLESHOT AND FOUND AILERON FEEL AND CENTERING MECHANISM SPRINGS WEAK. REPLACED NAMED SPRINGS IAW CMM 27-11-23. OPS CHECK GOOD IAW AMM B767 27-11-00 . AND RETURENED AC TO SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 73,180 hrs · 46,996 cycles

DURING CRUISE FLIGHT AT FL 360 WE PERFORMED APU CHECK AS APU CAME UP THE AUTO PILOT DISCONNECTED. RED A.P. DISCONNECT & SIREN RE-ENGAGED A.P., A.P. WAS NORMAL AT APPROX 26,000' WE GOT YELLOW AUTOPILOT DISCONNECT AND AUTOPILOT SISCRETE LITE. FULLY DISENGAGED A.P. CONTROLS WERE VERY HEAVY AND SLOW TO RESPOND. EMERGENCY DECLARED. GOT DELAYING VECTORS FOR ANOTHER APPROACH. LANDED SUCCESSFULLY WE GOT NO OTHER EICAS MESSAGES OR DISCRETE LITES. * LANDED IN SEA MTX GROUNDED AC AND DEFERRED CENTER AUTO PILOT IAW MEL ABX-22-10-1A AND RETURNED AC TO SERVICE .

Part: WARNING MESSAGE — FALSE INDICATION (NLG) · airframe 72,794 hrs · 46,816 cycles

DURING PUSH BACK, EICAS MSG "NOSE A/G DISAGREE' CAME ON A/C RETURNED INTO GATE AND MTX GROUNDED A/C . MTX PERFORMED NOSE WHEEL STERRING DRUM AND LOCKOUT INSPECTION CHECK, ACCOMPLISHED. IAW. AMM 32-34-05. NO DAMAGE NOTED A/C GOOD FOR SERVICE . MTX RETURNED AC TO SERVICE .

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 72,659 hrs · 46,751 cycles

DURING TAXI EICAS BULK CARGO DOOR MSG APPEARED AC RETURNED TO GATE AND MTX GROUNDED A/C , MTX CYCLED BULK BIN DOOR IAW AMM 52-36-01 OPS CK OK , RETURNED A/C TO SERVICE AND A/C DEPARTED

Part: PROXIMITY SENSOR — MALFUNCTIONED (THRUST REVERSERS) · airframe 72,638 hrs · 46,742 cycles

DURING TAKEOFF RH THUST REVERSER UNLOCK LIGHT CAME ON AND A/C ABORTRED TAKE OFF AND RETURNED TO THE GATE , MTX GROUNDED A/C AND DEFERRED THE RH T/R FOR DEPARTURE IAW ABX MEL 78-31-1 .AND RETURNED AC TO SERVICE . 7/13/24 MTX TROUBLESHOT IAW FIM 78-36 FAULT TREE 809 AND FOUND CODE 172 FAULTING S/66 REPLACED PROX SWITCH IAW 78-36-01. OPS CHECK GOOD ,AND CLEARED DI .

Part: CONTROL PANEL — INOPERATIVE (THRUST MANAGE) · airframe 72,535 hrs · 46,686 cycles

THRUST MANAGEMENT NUMBERS DON'T DISPLAY. DEFERRED. ACCOMPLISH MX PROCEDURE REVERSAL. T/S PER FIM 22-03 FT 803. NO DISCREPANCIES NOTED. H11 PARAMETERS PRESENT ON UPPER EICAS DUE TO LONG HISTORY, ITEM TO REMAIN DEFERRED. REMOVED AND INSTALLED SERVICEABLE THRUST MODE SELECT PANEL IAW AMM 22-31-02, OPS/CHK NORMAL. CLEARS DI #50770. PLACARD REMOVED, A/C REMAINS CAT 1 PENDING 30/40 TEST.

Part: SWITCH — FAILED (ELEVATOR FEEL) · airframe 55,988 hrs · 22,860 cycles

DURING TAXI ,ELEVATOR FEEL / STAB TRIM EICAS APPEARED. AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC. WHILE PERFORMING T/S WITH MCC FOUND PRESS SWITCH LEFT FAULTING ON SPM UNIT REPLACED SWITCH PER AMM 29-11-18. ALSO FOUND L HYD PUMP WITHOUT PRESSURE + WITHOUT L "SYS PRESS" LIGHT OR LOW "PRESS" LIGHT ILLUMINATES. NO HELP ON ORIGINAL ISSUE. T/S CONTINUES. CHECKED WIRES AT HYD PUMP REF WDM 29-11-12 + NO CONTINUITY FORUND ON PIN 2 OF UPPER HEAR SENSOR. NO POWER FOUND ON A/C CONNECTOR. T/S L HYD PUMP FLCU REF WDM 29-11-12, SSM 29-00-02, FOUND NO OUTPUT HOUR AT ELFU PER AMM 29-11-14. NO HELP, REINSTALLED ORIGINAL ELCU. T/S CONTINUES. SUSPECT PUMP AT FAULT. REPLACED L HYD DEMAND PUMP PER AMM 29-11-01, NO HELP. TRACED WIRE FROM OVERHEAT CANNON PLUG (D916) , FOUND LOOSE CANNON PLUG (D42808) TIGHTENED PLUG AND OPS CHECKED PER AMM 24-41-00 + AMM 27-31-00. STATUS MESSAGES CLEAR, OPS CHECKS NORMAL. NO FURTHER FAULTS AT THIS TIME.AC IS RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,434 hrs · 46,629 cycles

CAPTAIN REPORTED, ON FINAL APPROACH TO 33L BWI, GEAR DISAGREE AND NOSE GEAR LIGHT. WENT AROUND, ON DOWNWIND, NOSE LIGHT CAME ON. RAN NON NORMAL, LANDED NORMALLY.A/C WAS GROUNDED BY MAINTENANCE AND TROUBLESHOT ,BITE CHECK PSEU. TARGET 233 AND 255 ON BOX. TESTED TARGETS YHRU PSEU. BOTH NEAR. NO PROBLEMS WITH GEAR LIGHT ON GRD. CLEANED TARGETS AS PRECAUTIONARY REF FIM 32-09 FT 803. RETURNED A/C TO SERVICE FOR NEXT FLIGHT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,421 hrs · 46,624 cycles

A/T DISC WITH SPEED FLAG AND COULD NOT SET SPEEDS OR TO1. AC RETURNED TO GATE MAINTENACE GROUNDED A/C .PERFORMED RESET AND OPS CHECKED IAW AMM 22-32-00. OPS CHECK OK. AIRCRAFT RELEASED CAT I . AND RETURNED TO SERVICE,

Part: CIRCUIT BOARD — DEFECTIVE (MEC) · airframe 70,761 hrs · 46,109 cycles

BETWEEN 3000' AND 4000' MSL ON CLIMB OUT, CONFIG DISCREET LIGHT AND GEAR NOT DOWN EICAS MESSAGE WITH AURAL WARNING. THIS OCCURED WITH FLAPS UP AND LANDING GEAR UP.CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AIRPORT WITHOUT FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED PSEU BITE IAW FIM 32-09 FT 803 NO FAULTS FOUND. PERFORMED L,C,R RA BITE IAW FIM 34-33 FT 810 NO DEFECTS NOTED. PERFORMED FSEU BITE IAW FIM 27-51 FT 808. NO FAULTS FUND. PERFORMED L,C,R FSPM BITE IAW FIM 27-58 FT 804 NO DEFECTS NOTED. FOLLOWING FIM 31-51 FT 811, REMOVED AND REPLACED M983 LANDING CONFIGURATION MODULE IAW AMM 31-51-04. OPS CHECK OK. AICRAFT RETURNED TO SERVICE.

Part: CONTROL VALVE — SEIZED (ZONE 400) · airframe 70,686 hrs · 46,090 cycles

R/H ENG START VALVE INOP AFTER PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED + REPLACED RH ENG START VALVE IAW AMM 80-11-02. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 70,247 hrs · 45,954 cycles

CARGO DOOR CAUTION MESSAGE + DISCRETE LIGHT BULK CARGO DOOR. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESECURED BULK CARGO DOOR + VERIFIED OPERATION IAW B767 AMM 52-36-00. BULK CARGO DOOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 70,208 hrs · 45,940 cycles

AFTER ENGINE START RT ENGINE SHOWED N1 EXCEEDANCE 124.3 OUR START WAS NORMAL WITH NO EXCEEDANCE NOTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK ON N1 INDICATION IAW B767 AMM 77-12-01. NO FAULTS NOTED. INDICATION CLEARED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NOT ENTERED — NOT ENTERED · airframe 70,185 hrs · 45,933 cycles

AT PUSHBACK "CARGO DOORS" LIGHT ILLUMINATED. RETURNED TO GATE. THE LIGHT ON OVERHEAD PANEL IS WHAT CAME ON. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED BULK CARGO DOOR; OPS CK GOOD. ISSUE RESOLVED IAW B767 AMM 52-36-00. AIRCRAFT RETURNED SERVICE.

Part: STARTER — SPARKS (LEFT ENGINE) · airframe 70,060 hrs · 45,893 cycles

WHEN STARTING THE LEFT ENGINE, THE N2 HUNG UP @30% AND EGT HUNG AT 530*.ABORTED ENGINE START. AT MAINTENANCE REQUEST ATTEMPTED TO MOTOR ENGINE. NO N2 OBSERVED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED L/ENGINE STARTER PER AMM: 80-11-01. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSCREEN — CRACKED (ZONE 200) · airframe 69,902 hrs · 45,843 cycles

DURING FLIGHT R1 WINDOW CRACKED ACROSS FULL PANE. AIRCRAFT DIVERTED TO (LAS) AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED R1 WINDOW IAW 56-11-01. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — FAULTED (THRUST MANAGE) · airframe 69,664 hrs · 45,768 cycles

PRIOR TO ENG START, UNABLE TO INPUT DERATED THRUST OR ASSUMED TEMP. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THRUST MANAGEMENT COMPUTER IAW MEL 22-30-1A. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (STABILIZER) · airframe 69,355 hrs · 45,669 cycles

LOW SPEED ABORT ON TAKE-OFF FOR RED STABILIZER EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE RIGHT STAB INDICATION IAW MEL 27-48-1 CAT C CODE 11. PLACARD INSTALLED . AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — DEFECTIVE (RT FUEL SHUTOFF) · airframe 69,035 hrs · 45,571 cycles

RT. ENG FUEL VALVE MSG ON PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED #2 ENG CONDITIN CONTROL MOTOR ACTUATOR IAW B767 AMM 76-11-04. OPS CHECK GOOD AT THIS TIME. PERFORMED TROUBLESHOOTING IAW B767 FIM 76-11 FAULT TREE 807. C/W IDLE RUN IAW B767 AMM OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 68,852 hrs · 45,509 cycles

CONFIGURATION WARNING ON TKO STAB TRIM SET 6:8 (INSIDE GROUND BAND) UPON ADVANCING THRUST LEVERS FOR TAKEOFF WE RECEIVED A CONFIGURATION WARNING FOR FLAP CONFIGURATION. THE TRIM WAS SET CORRECTLY ACCORDING TO THE TLR. THE TRIM SETTING WAS 6.8 AND THE LIMIT OF THE GREEN ARC FOR THIS AIR FRAME WAS 7.0. THE CONFIGURATION WARNING WAS A FALSE ALARM BECAUSE THE TRIM WAS SET AND INSIDE THE GREEN ARC. I SUSPECT THE SWITCH POSITIONS FOR THE CONFIGURATION WARNING WE’RE NOT PRECISELY ALIGNED WITH THE GREEN ARC AS DEPICTED ON THE CAPTAINS SIDE OF THE PEDESTAL. FOR THE SECOND TAKEOFF WE ELECTED TO USE THE TRIM INDICATOR ON THE FIRST OFFICER SIDE WHICH WORKED JUST FINE. CREW ENTERED DISCREPANCY IN LOG BOOK UPON ARRIVING IN CVG. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE PERFORMED OPS CHECK OF TAKE OFF CONFIG WARNING ALERT IAW B767 AMM 31-51-00 OPS CHECK GOOD FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 67,724 hrs · 45,146 cycles

ANTI SKID EICAS MESSAGE ILLUMINATED ON TAXI. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. THE ANTI SKID SYSTEM WAS DEFERRED IAW MEL 32-42-1A AND THE AICRAFT WAS RETURNED TO SERVICE

Part: POWER SUPPLY — FAULTY (ZONE 100) · airframe 67,014 hrs · 44,913 cycles

SPEED BRAKES EXT EICAS MESSAGE DISPLAYED WITH SPEED BRAKES STOWED SPEED BRAKES LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED 2L CSEU P/S B767 AMM 27-09-00. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 66,968 hrs · 44,895 cycles

RIGHT EICAS COMPUTER STATUS MESSAGE APPEARED DURING TAXI. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED EICAS BITE CHECK AND CLEARED ALL FAULTS AND AIRCRAFT RETURNED TO SERVICE.

Part: FUSE — ACTIVATED (ZONE 700) · airframe 66,968 hrs · 44,895 cycles

ON TAKEOFF LEFT MAIN GEAR WOULD NOT RETRACT. GEAR DISAGREE & GEAR DOOR EICAS LIGHTS, AMBER "DOORS & GEAR ANNUNCIATORS ILLUMINATED LEFT MAIN GEAR LIGHT GREEN LANDING WEIGHT 271600 LBS, FLIGHT CREW DECIDED TO TURNBACK TO AIRPORT AND LANDED WITH NO ADDITIONAL PROBLEMS. MAINTENANCE GROUNDED THE AICRAFT. MAINTENANCE REMOVED AND REPLACED LEFT MAIN GEAR UP AND DOWN TRUCK FUSES IAW B767 AMM 32-32-19. ACCOMPLISHED LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL TEST IAW B767 AMM 32-32-00. NO DEFECTS NOTED, NO ABNORMAL NOISES NOTED, LANDING GEAR TIMES WITHIN LIMITS. AIRCRAFT RELEASED FOR FLIGHT.

Part: CONNECTOR — BURNED (EHSI INDICATOR) · airframe 66,801 hrs · 44,838 cycles

AIR TURN BACK CREW REPORTED SMOKE IN THE COCKPIT.EMERGENCY DECLARED. AIRCRAFT LANDED UNEVENTFULLY AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND SOURCE OF SMOKE TO BE CONNECTOR D109 ON CAPTAINS EHSI. MAINTENANCE REMOVED AND REPLACED AND REPINNED CONNECTOR D109 IAW BOEING SWPM 20-71-11. OPS CHECKED IAW B767 AMM 34-22-04. AIRCRAFT RELEASED FOR FLIGHT.

Part: DISPLAY — INOPERATIVE (EICAS) · airframe 66,568 hrs · 44,761 cycles

LOWER EICAS DISPLAY BLANKED BEFORE TAKE OFF, REAPPEARED AFTER VACATING RUNWAY. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED EICAS BITE PER FIM 31-41 BLOCK 45 NO FAULTS NOTED. AIRCRAFT RELEASED.

Part: ELECTRICAL BOX — FAULTED · airframe 65,975 hrs · 44,559 cycles

RANDOM ELECTRICAL ISSUES AFTER THE PLANE WENT DARK WHEN ONE OF THE RAMP EMPLOYEES ACCIDENTALLY PULLED THE POWER BEFORE AIR START OCCURRED ISSUES INCLUDED AUTOPILOT, AUTO THROTTLES, AUTO LAND GEAR. FLIGHT CREW WARE ABLE TO CLEAR MESSAGES AND DEPARTED ON TIME. AIRCRAFT TOOK OFF AND HAD MULTIPLE WARNINGS AND MESSAGES. FLIGHT CREW DECIDED TO PERFORM AIR TURNBACK. AIRCRAFT LANDED WITHOUT PROBLEM. AIRCRAFT WAS GROUNDED BY MAINTENANCE. PERFORMED PSEU TEST IAW B767 FIM 32-09, FT 803, BOX CAME BACK WITH CODE 403- SUBSYSTEM INPUT POWER FAILURE CONSISTENT W/ L REVERSER BEING ON DEFERRAL. NO OTHER ISSUES INDICATED. PERFORMED BPCU TEST IAW B767 FIM 24-20, FT 801, BOX CAME BACK WITH NO ISSUES. PERFORMED GROUND TEST 30 IAW B767 FIM 22-03, FT 818, TEST RESULTED IN NO ADDITIONAL FLIGHT FAULTS. PERFORMED GROUND TEST 40 IAW B767 FIM 22-03, FT 819. SYSTEM PASSED TEST, NO ISSUES. AIRCRAFT RELEASED FOR FLIGHT.

Part: EGT INDICATION — ACTIVATED (NR 2 ENGINE) · airframe 63,998 hrs · 43,742 cycles

AFTER STARTING #2, EGT INDICATOR DROPS TO 18C IN BOTH PRIMARY AND STBY DISPLAYS.AIRCRAFT WAS GROUNDED.

Part: ANGLE — WORN (NR 2 NACELLE) · airframe 63,909 hrs · 43,692 cycles

NR 2 OTBD FWD ZEE ANGLE WORN. THE AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO BAY) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO COMPARTMENT FLOORBOARD ATTACH FITTING CORRODED. THE AIRPLANE WAS GROUNDED.

Part: ANGLE — CRACKED (NR NAC FAIRING) · airframe 63,909 hrs · 43,692 cycles

NR 2 PYLON AFT FAIRING UPPER INBD AND OUTBD ANGLES CRACKED. THE AIRPLANE WAS GROUNDED.

Part: SEAL — WORN (NR 2 NACELLE) · airframe 63,909 hrs · 43,692 cycles

NR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.

Part: ATTACH ANGLE — GOUGED (NR 2 NACELLE) · airframe 67,509 hrs · 43,692 cycles

NR 2 PYLON AFT FAIRING, AFT BULKHEAD, LEFT AND RIGHT ATTACH ANGLES AREGOUGED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — WORN (NR 2 NACELLE) · airframe 63,909 hrs · 43,692 cycles

NR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO COMPARTMENT DOOR INTERIOR UPPER AFT WEB HAS LIGHT SURFACE CORROSION. THE AIRPLANE WAS GROUNDED.

Part: WEB — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO DOOR INTERIOR LOWER WEB UPPER CHORD CORRODED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FORWARD CARGO DOOR INTERIOR STRUCTURE 3RD CHORD FROM BOTTOM REMOVED CORRODED MINOR CHORD AND ASSOCIATED PARTS. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FORWARD CARGO COMPARTMENT DOOR INNER SKIN 2ND FROM BOTTOM CORRODED MINOR CHORD AND ASSOCIATED PARTS. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO DOOR INTERIOR LOWER FWD WEB HAS CORROSION. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (FWD CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FORWARD CARGO DOOR INTERIOR STRUCTURE 3RD CHORD FROM BOTTOM , BEHIND LIGHT SHROUD EXFOLIATION. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO DOOR INTERIOR LOWER AFT WEB HAS SURFACE CORROSION. THE AIRPLANE WAS GROUNDED.

Part: WEB — CORRODED (CARGO DOOR) · airframe 63,909 hrs · 43,692 cycles

FWD CARGO DOOR INTERIOR LOWER WEB STA 560 HAS CORROSION. THE AIRPLANE WAS GROUNDED.

Part: WARNING SYSTEM — NO TEST · airframe 63,782 hrs · 43,631 cycles

FIRE BELL AND CHIME WILL NOT TEST. AIRCRAFT WAS GROUNDED.

Part: ANNUNCIATOR — FAILED (COCKPIT) · airframe 63,149 hrs · 43,414 cycles

DURING BLOCKING IN AT THE GATE, THE CREW NOTICED SMOKE IN THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED). THE CAUSE OF THE SMOKE WAS THE LEFT ENGINE OIL PRESSURE ANNUNCIATOR THAT FAILED INTERNALLY. THE ANNUNCIATOR ASSEMBLY WAS REPLACED.

Part: SKIN — GOUGED (BS 522) · airframe 62,518 hrs · 43,166 cycles

GOUGE IN THE FUSELAGE SKIN AT FUSELAGE STATION 522, STRINGER 25R. THE GOUGE WAS CAUSED BY GROUND EQUIPMENT CONTACT. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: RETAINER — CORRODED (LT WING) · corrosion level 2 · airframe 59,890 hrs · 42,173 cycles

CORROSION ON THE LEFT WING LEADING EDGE NUTPLATE ASSEMBLY AT WS 446, WBL 300. THE NUTPLATE RETAINER WAS REPLACED. THE ACFT WAS GROUNDED.

Part: ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 59,890 hrs · 42,173 cycles

CORROSION ON THE LEFT WING LEADING EDGE NOSE FORMER ANGLE AT WS 456.975, WBL 310. THE ANGLE WAS REPLACED. THE ACCT WAS GROUNDED.

Part: ATTACH ANGLE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 59,890 hrs · 42,173 cycles

CORROSION ON THE LEFT MAIN LANDING GEAR WHEEL WELL UPPER SURFACE PANEL ATTACH ANGLE. THE ANGLE WAS REPLACED. THE ACFT WAS GROUNDED.

Part: ANGLE — CORRODED (BS 786) · corrosion level 2 · airframe 59,890 hrs · 42,173 cycles

CORROSION ON THE KEEL BEAM ANGLE AT BS 786, LBL 9 TO RBL 9. THE ANGLE WAS REPLACED. THE ACFT WAS GROUNDED.

Part: SUPPORT RIB — CORRODED (LT WING) · corrosion level 2 · airframe 59,890 hrs · 42,173 cycles

CORROSION FOUND ON THE LEFT WING UPPER AFT TRAILING EDGE PANEL SUPPORT RIB, WS 197.4, WBL 120. THE SUPPORT RIB WAS REPLACED. THE ACFT WAS GROUNDED.

Part: MEC — MALFUNCTIONED (LT ENGINE) · airframe 59,335 hrs · 41,964 cycles

LEFT ENGINE FLAME OUT (SHUTDOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 18,000 FEET. THE ENGINE WOULD NOT RESTART IN FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE'S MAIN ENGINE CONTROL (MEC), COMPRESSOR INLET TEMPERATURE (CIT) SENSOR, AND T2 SENSOR WERE REPLACED. THE CAUSE OF THE ENGINE SHUTDOWN WAS A FAULTY MEC, CIT SENSOR, AND/OR T2 SENSOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

AFT LOWER CARGO BILGE STATION 1395 - 1417, STRINGER 36L. WORK IS NOT AN SRM REPAIR. REWORKED REPAIR FROM 65269-0000-0953. PERFORMED REPAIR 2 IAW SRM 53-00-03. SDR INFO, CORRODED LEVEL 2, PART NAME STRINGER, SN N/A, FS & BS LOCATION FROM 1396 - 1417, STRINGER & WS LOCATION FROM STRINGER 36L - 36L. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

THE NR 7 OTBD ACTUATOR SUPPORT RIB HAS CORROSION IN THE ACTUATOR BORE. FINAL BORE SIZE IS 5.995 CLEAN & ROUND, NO DEFECTS NOTED, REA FORTHCOMING. REMOVED CORROSION FROM NR 7 OTBD ROTARY ACTUATOR SUPPORT, FINAL BORE SIZE 5.995". PERFORMED SURFACE SCAN IAW NDTM PART 6 51-00-19, NO DEFECTS NOTED. WORK DONE IAW REA B657-61972MR ACCOMPLISHED ON BACK. CORROSION LEVEL 2, PN 113T1345-24, NAME RIB HALF ASSEMBLY, LOCATION WS 729. ACFT WAS GNDED.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

LEFT WING OVERWING FUEL PORT FAILED BOND CHECK ON JC 28-018-00-01. REPAIRED AREA AT THE LT WING OVERWING FUEL PORT IAW REA B757-61987-MR. FUEL PORT PASSED BOND CHECK AFTER REPAIR WAS COMPLETED IAW AMM 28-11-04. CORRODED LEVEL 2, PN 112T3101-5, PART NAME NR 1 UPPER SKIN PANEL, SN NSN, FS & BS POSITION AT WS 798, STRINGER & WS FROM STRINGER 15 - 16. ACFT WAS GNDED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

MEC STATION 246, LBL 48.00, PLATFORM FWD WEB CRACKED, LOOSE & BENT. REPAIRED SUPPORT ASSEMBLY IAW SRM 51-70-11. FABRICATED REPAIR PARTS USING 2024T-3 .032", PO 0070726 & 2024 T-3 .040", PO 0080468 IAW SRM 51-70-11. CRACKED LENGTH 1.0", PN 284T0287-3, SN NSN, PART NAME SUPPORT, EXACT FS & BS LOCATION ON ACFT AT STATION 246, EXACT STRINGER & WS LOCATION ON ACFT AT LBL 48.0. ACFT WAS GNDED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

REFERENCE COI 62701-001, UPPER CARGO SEAT TRACK AT STATION 999, RBL 74.75, NEEDS REPLACED. REMOVED SEAT TRACK & MATCH DRILLED NEW SEAT TRACK WILL BE INSTALLED ON NR 0219. CRACKED 1.0", PN 368-53-00-95451-201, PART NAME SEAT TRACK CHORD, SN NSN, FS & BS LOCATION AT STATION 999, STRINGER & WS LOCATION AT RBL 74.75. ACFT WAS GNDED.

Part: BEAM — CRACKED (NR 1 PYLON) · airframe 56,535 hrs · 40,938 cycles

NUMBER ONE PYLON INBD BEAM, AT BOTTOM OF PANEL 437BR, IS WORN & CRACKED AT FWD END. REMOVED WORN & CRACKED BEAM & REPLACED WITH NEW BEAM IAW SRM 51-40-02. CRACKED LENGTH 1", PN 313T1380-243, SN NSN, PART NAME BEAM, EXACT FS & BS LOCATION ON ACFT FROM NAC STATION 364.93 TO 361.93, RBL.15.1, EXACT STRINGER & WS LOCATION ON ACFT FROM WS 340.3 - 0. ACFT WAS GNDED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

DEFERRED ITEM 84773 FROM LOG PAGE 36674-09 ENTRY 3. MCD POSITIONS A5R ,A6R ,M6, D7, E6 INOPERATIVE. STATION 999, RBL 74.75. R & R SEAT TRACK CHORD & FITTING IAW A DWG 368-53-00-95446. CRACKED 2.0", PN 368-53-00-95461-206, PART NAME FITTING, SN NSN, LOCATION STATION 999 LOCATION RBL 74.75. ACFT WAS GNDED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

THE RT FAILSAFE STRAP AT STATION 955 IS CRACKED AT LOWER FASTENER HOLE, COMMON TO T FITTING. REPAIRED RT FAILSAFE STRAP AT STATION 955 IAW DOCUMENT 47008ORD004 IAW JC EA 53500014-003. CRACKED .275", PN 145T2524-22, PART NAME FAILSAFE STRAP, SN NSN, FS & BS LOCATION AT STATION 955. ACFT WAS GNDED.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

RIGHT WING OVERWING FUELING PORT FAILED BOND CHECK ON JC 28-018-00-02. REPAIRED CORROSION UNDER FUELING PORT ON THE RT WING ON INSTALLED NEW FUELING PART & BOND TESTED GOOD IAW REA B657-61984-MR. CORRODED: LEVEL 2, PN 112T3101-6, SN NSN, PART NAME SKIN PANE NR 1. ACFT WAS GNDED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

CRACKED FITTING UNDER SEAT TRACK AT FS 654 & RBL 32. R & R CRACKED FITTING UNDER SEAT TRACK AT STATION 654 & RBL 32 IAW DWG 96F, 5667603, SEE BACK SIDE FOR PARTIAL WORK ACCOMPLISHED. SDR INFORMATION, CRACKED 1.2", PN 96F5667603-110, SN NSN, PART NAME LW LOBE CLIP, EXACT FS & BS LOCATION ON ACFT FROM FS 654 - 657, EXACT STRINGER & WS LOCATION ON ACFT FROM RBL 32 - RBL 32. ACFT WAS GNDED.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

AFT LOWER CARGO DOOR NR 5 BEAM CORRODED BEHIND LIGHT HOUSING MOUNT. R & R NR 5 BEAM IAW SRM 51-40-02. CORRODED LEVEL 2, PN 140T2605-3, SN N/A, PART NAME ALC DOOR BEAM NR 5, EXACT FS & BS LOCATION ON ACFT FROM FS 1285 - 1350, EXACT STRINGER & WS LOCATION ON ACFT, FROM STRINGER 17 - 16. ACFT WAS GNDED.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

AFT LOWER CARGO DOOR NR 7 BEAM IS CORRODED 36" FROM FWD EDGE. R & R NR 7 BEAM ON ALC DOOR IAW SRM 51-40-02. CORRODED LEVEL 2, PN 14OT2607-3, SN N/A, PART NAME ALC DOOR BEAM NR 7, EXACT FS & BS LOCATION ON ACFT, FROM 1285 - 1350, EXACT STRINGER & WS LOCATION ON ACFT, FROM STRINGER 17 - 17. ACFT WAS GNDED.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 56,535 hrs · 40,938 cycles

AFT LOWER CARGO DOOR NR 6 BEAM IS CORRODED 36" FROM FWD EDGE OF DOOR. R & R NR 6 BEAM IAW SRM 51-40-02. CORRODED, PN 140T2606-3, SN N/A, PART NAME ALC DOOR BEAM NR 6, EXACT FS & BS LOCATION ON ACFT FROM FS 1285 - 1350, EXACT STRINGER & WS LOCATION ON ACFT FROM STRINGER 16 - 15. ACFT WAS GNDED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

HEAVILY CORRODED AREA FOUND ON SKIN & TEAR STRAP FWD SIDE, STATION 1065, JUST BELOW STRINGER 13R. REPAIRED DAMAGED AREA IAW REA B653-61986MR. PN 145T3410-8, PART NAME SKIN, CORRODED LEVEL 2, EXACT FS & BS LOCSTION ON ACRAFT STATION 1065, EXACT STRINGER & WS LOCATED AT ON ACFT. STRINGER S13R.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

FRAME TO SKIN ATTACH ANGLE AT STATION 1417, LBL 12 CORRODED. R & R SHEAR TIE IAW SRM 51-40-02 4B & DWG 146T1216. CORRODED LEVEL 2, PN 146T1216-1, PART NAME SHEAR TIE, SN NSN, FS & BS LOCATION FROM 1417, STRINGER & WS LOCATION FROM 38L. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

HEAVILY CORRODED AREA ON SKIN & TEAR STRAP AT STATION 1065, FWD SIDE JUST BELOW STRINGER 8R. REMOVED STRINGER 8R FROM STATION 1065 - 1043 TO ACCESS CORROSION. BLENDED CORROSION, AREA WAS FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE WHEN COMBINING ON 145T0400. REPAIRED STRINGER 8R IAW SRM 53-00-03 FIG 201. CORRODED LEVEL 2, PN 145T3001-5, PART NAME STRINGER, SN NSN, FS & BS LOCATION AT STATION 1043. ACFT WAS GNDED.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

STRINGER SPLICE AT STRINGER 8R, STATION 1065, IS CRACKED ON THE UPPER AFT HAT FLANGE. FOUND AFTER STRINGER SPLICE WAS REMOVED ON NR 0884. R & R STRINGER SPLICE AT STATION 1065 & STRINGER 8R IAW SRM 51-40-02. CRACKED 2", PN 145T3001-5, PART NAME STRINGER SPLICE, SN NSN, FS & BS LOCATION FS 1065. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

NUMBER 1 FLAP SUPPORT TE OTBD ACTUATOR BORE HOLE HAS AREAS OF CORROSION. DEFECT NOTED IAW JC S57-798-24-01. REPAIRED BORE HOLE IAW REA B657-61988-MR. CORROSION REMOVED IAW SRM 51-10-02. CORRODED LEVEL 2, PN 113T1345-19, PART NAME RIB HALF, SN NSN, WS LOCATION AT LEFT WS 801 - 801. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

NUMBER 1 TE FLAP SUPPORT, INBD ACTUATOR, BORE, HOLE HAS EVIDENCE OF CORROSION DEFECT. NOTED REF JC S57-798-24-01 STEP 2 & 3. REPAIRED IAW REA B657-61988-MR. CORRODED LEVEL 2, PN 113T1345-21, PART NAME RIB HALF, SN NSN, WS LOCATION AT LT WS 795. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

NUMBER 2 FLAP SUPPORT TE OTBD ACTUATOR BORE HOLE HAS CORROSION & TOOLING MARKS, DEFECTS NOTED IAW JC S57-798-24-01 STEP 2 & 3. REMOVED CORROSION FROM BORE IN 20BD ACTUATOR BORE IAW SRM 51-10-02. FINAL SIZE 6.048, REAMED DAMAGE HOLE IAW REA B657-61989-MR. IN ADDITION SEE PARTIAL WS 44. PN 113T1345-23, PART NAME RIB HALF, SN NSN, CORRODED LEVEL 2, EXACT STRINGER & WS LOCATION OAC, WS 619 - 619. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

NUMBER 2 FLAP SUPPORT TE INBD ACTUATOR BORE HOLE HAS CORROSION & TOOLING MARKS, DEFECTS NOTED IAW JC S57-798-24-01 STEP 2 & 3. REPAIRED IAW REA B657-61989-MR. CORRODED LEVEL 2, PN 113T1345-25, PART NAME RIB HALF, SN NSN, WS LOCATION FROM WS 613 - 613. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

RIGHT WING LE AIR LOAD RIB CORRODED AT WS 479. R & R RT WING LE AIR LOAD RIB AT WS 479 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-14, PART NAME STRUT RIB, SN NSN, WS LOCATION FROM WS 479 - 479. ACFT WAS GNDED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

AFT BULK CARGO, STATION 1417, ABOVE STRINGER 36L, FLOORBEAM STIFFENER CRACKED. R & R STIFFENER IAW SRM 51-40-02 4B & 7D, DWG 146T1216, CRACKED 1.5". PN 146T1261425, PART NAME STIFFENER, SN N/A, FS & BS LOCATION FROM 1417, STRINGER & WS LOCATION FROM 36L. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

LEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 575, OTBD OF NR 4 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R AIR LOAD RIB AT OSS 575 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2209-17, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 575 - 575. ACFT WAS GNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

AFT BULK CARGO, BILGE STATION 1417, STRINGERS 32R & 33R, INTERSECTION OF TOP OF FLOORBEAM & FLOOR SUPPORT CORROSION. R & R FLOORBEAM IN ALC BULK CARGO STATION 1417, STRINGER 32R - 33R, AT TOP OF FLOORBEAM & FLOOR SUPPORT IAW SRM 51-40-02. PN 452T3230-14, PART NAME BEAM, CORRODED LEVEL 2, EXACT LOCATION ON ACFT 1415 - 1417, EXACT WS LOCATION ON ACFT LBL 41 TO RBL 41. ACFT WAS GNDED.

Part: BEAM — CRACKED (RT WING) · airframe 56,535 hrs · 40,938 cycles

BEAM BELOW HYD BAY ACCESS DOOR 447BR CHAFED & CRACKED AT FWD END. REMOVED OLD BEAM & INSTALLED NEW BEAM IAW 51-40-02. CRACKED 1", PN 313T1380-209, SN NSN, PART NAME BEAM, EXACT FS & BS LOCATION ON ACFT, ENG BS O.OO - 10.0, EXACT STRINGER & WS LOCATION ON ACFT WS 344.3. ACFT WAS GNDED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

INNER CHORD HAS 0.125 CRACK AT LFS 859.5, LBL 89. REFERENCE JC NEA53000045-001 FOR DETAILS. REPAIRED INNER CHORD AT LFS 859.5, LBL 89 IAW JC NEW 53000045-01 & EA 53000047-101. CRACKED LENGTH .125", PN 145T1001-1, SN NSN, PART NAME INNER CHORD, EXACT FS & BS LOCATION ON ACFT, FROM STATION 859.5 - 859.5. EXACT STRINGER & WS LOCATION ON ACFT, FROM LBL 89 - 89. ACFT WAS GNDED.

Part: SPAR — GOUGED (RT WING) · airframe 56,535 hrs · 40,938 cycles

NUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 2 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657-31981 MR. GOUGE PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION: WS 789. ACFT WAS GNDED.

Part: SPAR — GOUGED (RT WING) · airframe 56,535 hrs · 40,938 cycles

NUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 1 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B657-61981-MR. GOUGE, PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE 749 RT WING, FS & BS LOCATION WS 798. ACFT WAS GNDED.

Part: SPAR — GOUGED (RT WING) · airframe 56,535 hrs · 40,938 cycles

NUMBER 8 FLAP SUPPORT RIB AT REAR SPAR, PERFORMED FASTENER HOLE INSPECTION AT NR 4 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B65731981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION WS789 RT WING. ACFT WAS GNDED.

Part: SPAR — GOUGED (RT WING) · airframe 56,535 hrs · 40,938 cycles

NUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 3 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657 -61981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING, FS LOCATION, WS 789. ACFT WAS GROUNDED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,535 hrs · 40,938 cycles

INNER CHORD HAS 0.250 CRACK AT RFS 883.5, RBL 89. REFERENCE JC NEA 53000048-001 FOR DETAILS. REPAIRED CRACK ON INNER CHORD AT RFS 883.5, RBL 89 IAW NEA 53000048-001 & EA 60361. CRACKED, LENGTH 0.250", PN 145T1004-2, PART NAME INNER CHORD, SN NSN, FS & BS LOCATION, FROM 883.5 - 883.5, STRINGER & WS LOCATION, FROM RBL 89 - 89. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 56,535 hrs · 40,938 cycles

LEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 884, OTBD OF NR 2 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R RIB IAW SRM 51-40-02 7D & DWG 114T222. CORRODED LEVEL 2 PN 114T2222-15, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 884 - 884. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,783 hrs · 39,803 cycles

STATION 676 18L STRINGER CRACKED. REPAIRED CRACKED STRINGER 18L AT STATION 676 IAW REA B653-61104-MR. PN 143T3001-12, PART NAME STRINGER 18L, CRACKED 1 INCH, EXACT FS FROM 682, EXACT STR LOC ON ACFT 18L. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,783 hrs · 39,803 cycles

RIGHT WING TE TRANSVERSE BEAM AT WS 285 CORRODED SEVERAL SPOTS ALONG INBD EDGE JUST UNDER PANEL 651MT. R & R RT WING TE TRANSVERSE BEAM IAW SRM 51-40-02 & REA NR B657-61111. SDR INFO PN 113T1623-126, PART NAME UPPER CHORD, SN NA, CORRODED LEVEL 2. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 54,783 hrs · 39,803 cycles

RIGHT WING LE RIB CORRODED AT WS 478. REMOVED CORRODED RIB & INSTALLED FABRICATED RIB IAW REA B657-61105 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-16 PART NAME AIR LOAD RIB STRUT, SN NSN, STR & WS LOC RT WING STATION OSS 479.854 TO OSS 479.854 LE. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,783 hrs · 39,803 cycles

STATION 676 19L STRINGER CRACKED. R & R STRINGER 19L STATION 682 IAW SRM 53-00-03 & REAS B653-61104-MR. CRACKED 1 INCH. PN 143T3001-17, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT FS 682, STR & WS LOC ON ACFT STR 19L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,783 hrs · 39,803 cycles

STATION 676 8L STRINGER CRACKED. R & R STRINGER 8L STATION 676 IAW SRM 53-00-03 & REA B653-61104-MR. CRACKED 1.75 INCHES, PN 143T3001-6, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT FS 682, STR & WS LOC ON ACFT STR 8L. ACFT WAS GNDED.

Part: SPAR WEB — CORRODED (RT WING) · corrosion level 2 · airframe 54,783 hrs · 39,803 cycles

FRONT SPAR WEB CORRODED AFT OF NR 5 SLAT AT LES 450. REPAIRED FRONT SPAR WEB AFT OF NR 5 SLAT AT LES 450 IAW REA B657-61106-MR. PN 112T2007-1, PART NAME SPAR WEB, SN NSN, CORRODED LEVEL 2, EXACT WS LOC ON ACFT 448 TO 452. ACFT WAS GNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 53,774 hrs · 39,228 cycles

FRAME FAILSAFE CRACKED AND CORRODED. CRACK VERIFIED WITH HFEC IAW NDTM, PART 6 51-00-19 AND VISUALLY VERIFIED. FAILSAFE REPAIRED ON JC EA53500013-003. ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 53,774 hrs · 38,228 cycles

FAILSAFE CRACKED 1.7", LEFT FS 955, LBL 85.9. AIRCRAFT WAS GROUNDED. REPAIRED IAW REA B653-60654-MR.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,774 hrs · 39,228 cycles

OTBD FWD CORNER OF PRESSURE WEB CRACKED JUST AFT OF SIDE FRAME ATTACH FLANGE. FABRICATED NEW WEB IAW DWG 145T8752 INSTALLED IAW EA 53500013-003, PG. 10, STEP 25.

Part: SKIN — SEPARATED (RT AILERON) · airframe 53,403 hrs · 39,017 cycles

RIGHT OUTBOARD AILERON UPPER SURFACE SKIN SEPERATED AND PEELED BACK. RIGHT OUTBOARD AILERON REPLACED. REMOVED AND REPLACED RIGHT OUTBOARD AILERON, ACFT WAS GROUNDED.

Part: ANGLE — CORRODED (LT WING) · airframe 53,003 hrs · 38,755 cycles

DURING A HEAVY MAINTENANCE INSPECTION, TWO RAISED AREAS NOTED ON TOP SURFACE OF WING TRAILING EDGE FORWARD OF NUMBER 6 SPOILER. AREA OF THE LEFT WING UPPER CHORD (PN113T1406-7) FORWARD OF THE NR 6 SPOILER (WS 227 TO WS 314) FOUND CORRODED. FABRICATED REPAIR CHORD USING BAC1506-2633-7075-T6511 AND INSTALLED PER BOEING 767 SRM 51-40-05 AND 51-40-02. WORK ACCOMPLISHED ON WO #600320264 AND N774AX-57 WO 32816; ACFT WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,273 hrs · 37,773 cycles

FUSELAGE SKIN CRACKED AT FS 1702, STRINGER 6L. CRACK IS .25 INCH LONG. REPAIRED DAMAGE AT FUSELAGE STA 1702, STRINGER 6L IAW B767 SRM 53-00-01. PRIMED AREA IAW B767 51-21-10-7.

Part: FIRESEAL — CRACKED (NR 2 ENGINE) · airframe 51,273 hrs · 37,773 cycles

NR 2 ENGINE OUTBOARD REVERSER INBOARD AFT FIRE SEAL MATING SURFACE IS CRACKED. REPAIRED AREA IAW B767 SRM 51-70-13.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 51,273 hrs · 37,773 cycles

NR 1 ENG AFT MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT FROM STEP G1 TO G3 IAW AMM 71-2-04.

Part: FLOORBEAM — CORRODED (BS 1402) · airframe 48,703 hrs · 36,234 cycles

FLOOR SUPPORT CORRODED AT FS 1402, LEFT BUTT LINE 21. REMOVED, REPAIRED AND REINSTALLED FLOOR SUPPORT IAW B767 51-70-12 AND 51-40-O2.

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,703 hrs · 36,234 cycles

LOWER FORWARD CORNER OF THE R1 DOOR HAD A CRACKED BEAM. REPAIRED AREA IAW REA B652-55550-MR.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 48,526 hrs · 36,165 cycles

HYDRAULIC QUANTITY DECREASED TO .46 QTY STABLE WITH EDP DEPRESSURIZED ACMP OFF. OPENED COWLINGS, SERVICED RIGHT HYDRAULIC SYSTEM IAW B767 MM. RIGHT ENGINE FOUND FLUID LEAK AT STRUT DISCONNECTOR, REPLACED O-RING. NO LEAKS NOTED.

Part: CIRCUIT CARD — FAULTY (SMOKE DETECTION) · airframe 47,172 hrs · 35,658 cycles

MAIN CARGO SMOKE DETECTION SYSTEM FAILS SELF TEST. REMOVED AND REPLACED AFOLTS CARD M2026 IAW FIM 26-14-00 AND OPS CHECK GOOD IAW MM 26-14-00.

Part: RIB — CORRODED (LT WING) · airframe 46,486 hrs · 35,389 cycles

LT WING LEADING EDGE RIB AT STA. WA 920 (APPROXIMATELY) HAD EXFOLIATED CORROSION AT FORWARD END AND LOWER FLANGE LOWER SURFACE. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-01.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 45,979 hrs · 35,189 cycles

LIFE RAFT SLIDE DEPLOYED WITHOUT BEING ARMED. THE LOWER FORWARD ENTRY DOOR HUNG WHILE TRYING TO CLOSE IT. WHEN THE DOOR WAS RAISED FOR RE-CLOSURE, THE SLIDE DEPLOYED. INSPECTED DOOR AND GIRT BAR ATTACHMENTS. NO DEFECTS NOTED. REMOVED AND REPLACED SLIDE ASSEMBLY IAW B767 MM 25-66-01.

Part: STRUCTURE — VIBRATION (AIRFRAME) · airframe 44,373 hrs · 36,639 cycles

AIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 280 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE INDICATIONS WERE NORMAL. VIBRATION WAS EVIDENT IN SEAT AND FLOOR OF COCKPIT. NO OSCILLATION/VIBRATION WAS FELT IN THE FLIGHT CONTROLS. ALTITUDE WAS 11,000 FEET THROUGH FL330. AT CRUISE, FL 350, .8A M, VIBRATION IS NOT NOTICEABLE. VISUAL INSP OF HORIZ, STAB JACKSCREW AND SURROUNDING AREA, NO DEFECTS NOTED. RAN STAB THROUGH FULL RANGE OF MOVEMENT. CHECKED GOOD. PERFORMED MXSP TEST 68. STAB CHECK GOOD. FUNCTIONAL CHECK FLIGHT PERFORMED. ALL SYSTEMS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,646 hrs · 34,025 cycles

WHEN TESTED EMERGENCY LIGHTS, LIGHT OVER COCKPIT DOOR WAS INOP. TWO EACH LIGHTS AT ENTRANCE DOOR GOOD. ALSO, SPARE LIGHT SUPPLY INOP. REPLACED MAIN EMERGENCY BATTERY POWER SUPPLY IAW B767 AMM 33-51-07. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,602 hrs · 33,362 cycles

DURING MAINTENANCE TEST OF EMERGENCY LIGHTING SYSTEM, FOUND STANDBY BATTERY INOPERATIVE. INSTALLED NEW BATTERY PACK IAW B767 MM 33-51-07-02. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 40,602 hrs · 33,362 cycles

DURING MAINTENANCE INSPECTION, FOUND BOTH EMERGENCY LIGHTS INOPERATIVE. REPLACED PRIMARY EMERGENCY LIGHT POWER SUPPLY AND TESTED IAW B767 MM 33-51-07. PRIMARY SUPPLY OPS CHECKED GOOD. LIGHTS ILLUMINATED.

Part: SLAT — DELAMINATED (WING) · airframe 38,031 hrs · 32,556 cycles

NR 1 SLAT T/E WEDGE IS DELAMINATED ON THE INBD EDGE. REPAIR PER ER/A 380633-14AD