N744AX

Part: FIRE WARNING — ILLUMINATED (ZONE 400) · airframe 104,725 hrs · 46,789 cycles

INTERMITTENT #2 ENG FIRE LOOP STATUS MESSAGE DURING FLIGHT. FOQA DATA SHOWS THE LOOP IS FAULTING INTERMITTENTLY IN DESCENT. DOES NOT FAULT IN TAKE OFF OR CRUISE. DEFERRED RH ENG FIRE LOOP 2 PER MEL 26-11-1-1, MX ACTION C/W, PLACARDS INSTALLED, AC REMAINS NO ETOPS, MBCB 01/07/26. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — FAULT MESSAGE (ZONE 400) · airframe 104,717 hrs · 46,786 cycles

RIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE ILLUMINATED. DEFERRED RT ENG FIRE LOOP 2 PER MEL 26-11-14. MAINTENANCE ACTION C/W PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAULTED (ZONE 700) · airframe 104,701 hrs · 46,771 cycles

THERE IS UNUSUALLY LONG GEAR EXTENSION (RIGHT MAIN) DURING APPROACH WITH SHORT EICAS MESSAGE "GEAR DISAGREE", DISAPPEARED SOON.AFTER LANDING IN CVG MTX GROUNDED A/C AND DEFERRED LANDING GEAR ACTUATION SYSTEM IAW MEL 32-30-1. REPO"D AC TO ILN FOR TROUBLE SHOOTING.ILN MTX JACKED A/C AND REMOVED AND REPLACED RH MLG RETRACT ACTUATOR IAW AMM 32-32-01 AND LH MLG SIDE BRACE ACTUATOR IAW B767 AMM 32-32-02.PERFORMED GEAR SWINGS IAW B767 AMM 32-32-00. ALL OPS AND LEAK CHECKS GOOD VERIFIED ALL GEAR OPERATE WITHIN LIMITS THIS CLEARS DI.REACTIVATION PROCEDURES ACCOMPLISHED PLACARDS REMOVED .RII FORMS 32-01-1 AND 32-02-1 ACCOMPLISED. A/C RETURNED TO SERVICE.

Part: FIRE LOOP — FAULTED (ZONE 400) · airframe 104,699 hrs · 46,769 cycles

R ENG FIRE LOOP 2 STATUS MSG APPEARED SEVERAL TIMES ENROUTE AND BLANKED AFTER A MINUTE EACH TIME. AFTER LANDING MTX DEFERRED RT ENG.LP2 IAW MEL 26-11-1-1 NO MAINTENANCE PROCEDURES REQ AC REMAINS NO ETOPS. RETURNED AC TO SERVICE.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 104,563 hrs · 46,702 cycles

DURING TAXI, RIGHT ENGINE OIL QUANTITY INDICATION INOP. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE OIL QTY. INDICATION IAW MEL 79-31-1-1. MBCB 11/02/2025. REPETITIVE INSPECTION REQUIRED BEFORE EACH FLIGHT. AIRCRAFT RETURNED TO SERVICE.

Part: BLEED VALVE — WARNING MESSAGE (RT ENGINE) · airframe 104,483 hrs · 46,657 cycles

ON T/O ROLL, (R ENG BLEED VAL) CAUTION MSG APPEARED. ABORTED TAKE-OFF AT 68 KNTS AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C .MTX DEFERRED RH ENGINE BLEED IAW MEL ABX - 36-11-2-1. AND RETURNED A/C TO SERVICE.

Part: FUSE — DEFECTIVE (ZONE 200) · airframe 104,378 hrs · 46,619 cycles

DURING TAXI, R HYD SYSTEM QUANITY LOW. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REMOVED AND REPLACED HYDRAULIC FUSE ON RH ANTISKID MODULE OUT "D" POSITION. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (ZONE 900) · airframe 104,299 hrs · 46,600 cycles

DURIING FLIGHT, LOW BATTERY CHIRP ON LAV SMOKE DETECTOR. MAINTENANCE REPLACED LAV SMOKE DETECTOR BATTERY IAW AMM SUPP 26-12-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — INTERMITTENT (ZONE 400) · airframe 104,215 hrs · 46,574 cycles

RIGHT ENGINE FIRE LOOP 2 MSG ON DESCENT INTERMITTENT. OPENED COWLS AND CHECKED FIRE LOOP, FOUND OK. DEFERRED IAW MEL C ABX-26-11-1-1. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — FAULTED (LEFT ENGINE) · airframe 104,052 hrs · 46,517 cycles

ON TAKE-OFF AND ENGINE START, LEFT ENG DID NOT DISPLAY N1 IDICATION. AIRCRAFT ABORTED TAKE-OFF. (ATO). REMOVED AND REPLACED LT ENG N1 SPEED SHAFT SENSOR IAW B767 AMM 77-12-01, NO HELP. PERFORMED T/S PER WDM 77-12-11. FOUND CONNECTOR D4224P UNSECURED. RE-SECURED PLUG IAW SWPM 20-60-00. OPS CHECKED GOOD IAW 77-12-01. AIRCRAFT RETURNED TO SERVICE.

Part: EXHAUST VALVE — FAULTED (ZONE 100) · airframe 104,045 hrs · 46,512 cycles

ON CLIMBOUT, FWD EQPT VAL EICAS MESSAGE WOULD NOT EXTINGUISH. CONTACT MX CONTROL, RETURNED TO MIA. (ATB) DEFERRED FWD EQPT EXHAUST VALVE IAW MEL 21-58-7-2-1. MX C/W 21-58-7. PLACARD INSTALLED MBCB 06/26/25. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: BLOWOUT PANEL — MISSING (ZONE 400) · airframe 103,930 hrs · 46,478 cycles

DURING INSPECTION AT MIA, MAINTENANCE FOUND ON RIGHT ENGINE ON O/B SIDE OF RADIANT HEAT SHIELD BLOW OUT PANEL MISSING. INSTALLED NEW BLOW OUT PANEL "RADIANT HEAT SHIELD" ON O/B SIDE OF RIGHT ENG IAW AMM 72-31-00. A/C REMAINS NO ETOPS. DEFERRED MISSING LANYARD PER ABX-REA-7200-65769-00 AND GMM 07.04 FOR MX TRACKING. MBCB 06-30-2025. CONFIRMED ON RH ENGINE HEAT SHIELD TO BE INSTALLED AND HARDWARE PRESENT IAW ABX-REA-7200-65769-00. THIS CLEARS DI# 62794. PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 103,930 hrs · 46,478 cycles

AFTER BLOCK OUT WITH BOTH ENGINES RUNNING AND FLAPS EXTENDED EICAS MESSAGE APPEARED CENTER 1 PRIMARY PUMP ALSO PRESSURE LIGHT ON C1 PUMP. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED SYSTEM IAW MEL C ABX-29-31-2-1. PERFORMED OPS CHECK OF C1 AND C2 HYD SYSTEM IAW AMM 29-11-00. OPS CHECK GOOD. SWAPPED PRESSURE SWITCHES IN PRECAUTION IAW AMM 29-11-09. OPS CHECK GOOD. NO LEAKS DETECTED. THIS CLEARS DI 29849. PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: BLOWOUT PANEL — MISSING (ZONE 400) · airframe 103,930 hrs · 46,478 cycles

DURING INSPECTION AT MIA, MAINTENANCE FOUND ON LEFT ENGINE ON I/B SIDE OF RADIANT HEAT SHIELD BLOW OUT PANEL MISSING. INSTALLED NEW BLOW OUT "RADIANT HEAT SHIELD" ON I/B SIDE OF LEFT ENG IAW AMM 72-31-00. A/C REMAINS NO ETOPS. DEFERRED MISSING LANYARD PER ABX-REA-7200-65745-00 AND GMM 07.04 FOR MX TRACKING. MBCB 06-30-2025. CONFIRMED ON LH ENG HEAT SHIELDS TO BE INSTALLED AND HARDWARE PRESENT IAW ABX REA-7200-65745-00. THIS CLEARS DI# 62793. PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: COOLING FAN — FAULTED (ZONE 100) · airframe 103,274 hrs · 46,235 cycles

DURING TAXI ,EICAS "FWD EQUIP OVHT: DESCREET LT "OVHT", WENT TO STBY AND BOTH INDICATIONS RETURNED AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED FWD EQUIP. COOLING IAW MEL-ABX-21-58-1-1 . FOR DEPARTURE AND RETURNED AC TO SERVICE

Part: OIL SYSTEM — LOW (LT ENGINE) · airframe 103,217 hrs · 46,211 cycles

AFTER BLOCK OUT, ON ENGINE STARTS & ENGINES RUNNING 8 MINUTES (APPROX) LEFT ENGINE QUANTITY 11, RIGHT ENGINE 14, CONTACTED MAINTENANCE & TOLD TO RETURN TO GATE FOR SERVICING. MAINTENANCE GROUNDED THE AIRCRAFT. MAINTENANCE SERVICED LEFT ENGINE OIL IAW 767-AMM 12-31-01. CAPS AND ACCESSS PANEL VERIFIED CLOSED. AIRCRAFT RETURNED TO SERVICE.

Part: BEAR STRAP — CORRODED (ZONE 100) · airframe 103,174 hrs · 46,193 cycles

DURING N744AX C-CHECK AT AIRBORNE (TAMPA), THE LH BULK CARGO DOOR SURROUND STRUCTURE, BEAR STRAP P/N 146T8220-1 BETWEEN STA 1395-1417 AND STR 33L HAS CORROSION. THE DAMAGE WAS REMOVED BY BLEND-OUT PROCESS. THE ORIGINAL THICKNESS IS 0.160 INCHES AND THE REMAINING MATERIAL IS 0.118 INCHES AFTER BLENDED PROCESS. THE BEAR STRAP DOUBLER IS FABRICATED FROM 2024-T3 AL ALLOY. THERE ARE NO REPAIRS AND/OR ALLOWABLE DAMAGE FOR THE SPECIFIC LOCATION IN THE 767-200 SRM. THEREFORE, FVCI WAS CONTACTED TO REQUEST PERMANENT REPAIR INSTRUCTIONS. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE NOTED CONDITION AS APPROVED BY FVCI 8110-3.ACCOMPLISHED REPAIR ENGINEERING AUTHORIZATION REA # ABX-REA-5365-65336-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 103,112 hrs · 46,171 cycles

AFTER PUSHBACK C HYD PRIM 1 EICAS MESSAGE APPEARED JUST AFTER PUSHBACK AND BOTH ENGINES STABILIZED A/C RETURNED TO THE GATE AND MTX GROUNDED A/C . MTX VERIFIED HYD PUMP WORKING. REF AMM 29-11-00. OPS CHECK GOOD. AND RETURNED A/C TO SERVICE.

Part: VALVE — FOD (NR 2 ENGINE) · airframe 102,983 hrs · 46,103 cycles

DURING TAXI AFTER #2 ENGINE START, ENGINE STABILIZED, SPAR VALVE DISCRETE LIGHT ILLUMINATED, #2 ENGINE SHUT DOWN.AND AC RETURNED TO GATE .MAINTENANCE GROUNDED AC AND FOUND PART OF OLD CLAMP JAMMING VALVE ARM. REMOVED FOD AND OPS CK GOOD IAW AMM 28-22-11.AC WAS RETURNED TO SERVICE AND DEPARTED.

Part: VALVE — LEAKING (HYD SYSTEM) · airframe 102,980 hrs · 46,101 cycles

AFTER PUSHBACK R HYD SYS PRESS EICAS MESSAGE AND DISCRETE LIGHT ILLUMINATED AFTER SETTING BRAKES AFTER PUSH-BACK. R HYD STS QUANTITY ON STATUS PAGE READS 0.00RF.AC RETURNED TO GATE AND SHUT DOWN ,MAINTENANCE GROUNDED AC .AND FOUND NBR ONE MLG BRAKE HYDRAULIC FUSE HOUSING CRACKED. REPLACED FUSE IAW B767 AMM 32-42-03. SERVICED HYDRAULICS ,OPS AND LEAK CHECKS GOOD. A/C REMAINS CAT 3A OPERATIONAL. AC WAS RETURNED TO SERVICE .

Part: BATTERY — UNSERVICEABLE (APU) · airframe 102,893 hrs · 46,072 cycles

DURING TAXI APU INOP. AC RETURNED TO GATE AND MAINTENANCE GROUDED AC .DEFERRED FOR DEPARTURE AND RETURNED AC TO SERVICE . NEXT LEG MAINTENANCE REPLACED APU BATTERY AND OPS CHECKED GOOD . "

Part: APU — INOPERATIVE (ZONE 100) · airframe 102,893 hrs · 46,072 cycles

APU INOP

Part: BATTERY — UNSERVICEABLE (MAIN) · airframe 102,892 hrs · 46,071 cycles

AMENDED ,"DURING TAXI MAIN BATT CHARGER STATUS MESSAGE AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC , DEFERRED APU AND SWAPPED BATERY FOR DEPARTURE IAW 24-31-01 AND APU DEFERRAL ABX-49-11-1A AND RETURED A/C TO SERVICE "

Part: BATTERY — FAILED (MAIN) · airframe 102,893 hrs · 46,072 cycles

MAIN BATT CHARGER STATUS MESSAGE

Part: INDICATOR — MALFUNCTIONED (MLG) · airframe 102,351 hrs · 45,885 cycles

SELECTED GEAR DOWN AND RIGHT LANDING GEAR INDICATION DOES NOT SHOW DOWN AND LOCKED. NO EICAS MESSAGE DISPLAYED. DECLARED AN EMERGENCY. LANDED SAFELY. TAXIED CLEAR OF RUNWAY INSTALLED GEAR PINS AND TOWED TO GATE.MAINTENANCE GROUNDED AC AND TROUBLESHOT FINDING RIGHT LANDING GEAR INDICATION LIGHT INOP. REMOVED AND REPLACED RIGHT LANDING GEAR INDICATION BULBS IAW B767 AMM 33-16-02. OPS CHECK GOOD. MLG INDICATIONS GOOD. INSPECTED MLG I AW B767 AMM 32-11-01. NO DEFECT NOTED AC RETURENED TO SERVICE.

Part: PITOT TUBE — MALFUNCTIONED (ZONE 200) · airframe 102,307 hrs · 45,872 cycles

AFTER STARTING NUMBER 2 ENGINE WHILE TAXI OUT CAPTAIN PITOT STATUS AND OVERHEAD CAPTAIN PITOT LIGHT CAME ON. AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . TROUBLE SHOT AND REMOVED AND REPLACED CAPTAINS PITOT STATIC PROBE IAW B767 AMM 34-11-01. PERFORMED LEAK TEST IAW B767 AMM- 34-11-01-00-73-811 AND 34-11-01-00-730-804. LEAK TEST GOOD.AC WAS RETURNED TO SERVICE FOR DEPARTURE .

Part: UNKNOWN — UNSERVICEABLE (ZONE 100) · airframe 101,673 hrs · 45,676 cycles

L IRS FAULT LIGHT ILLUMINATED WHEN TAXIING FOR TAKE OFF AC BTB GROUNDED AND DEFERRED IAW ABX-34-21-1-1-1A ,A/C FLOWN TO SBD MX,GROUNDED AC REMOVED AND REPLACED LEFT IRU IAW AMM 34-21-01. IRU TEST PASSED. MCDP TEST 30 SHOWED NO FAULTS. THIS CLOARS DI 45871. PLACARDS REMOVED. NO REACTIVATION PROCEDURES APPY. A/C RALM DOWNGRADED TO CAT 1, PENDING MCDP TESTS 30 & 40. REF LP : 38658-62/3.AC RETURNED TO SERVICE

Part: BLEED VALVE — FAULTED (RIGHT ENGINE) · airframe 101,128 hrs · 45,508 cycles

RIGHT ENGINE BLEED OFF EICAS. NO DUCT PRESSURE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED #2 ENGINE PRSOV IAW B767 AMM 36-11-09. ENGINE RUN REFORMED AND PNEUMATIC SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE,

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,439 hrs · 45,310 cycles

WX RADAR FAIL ON TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF WEATHER RADAR IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,420 hrs · 45,306 cycles

AFTER ENGINE START "FWD EQPT VAL" EICAS AND VALVE DISCRETE LIGHT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND OVRBD VALVE C OUT, RESET CB + RUN BOTH ENGINES PER B767 AMM 71-00-00 OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 100,174 hrs · 45,227 cycles

EICAS MESSAGE C HYD PRIM 1 ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL TEST AND IDLE ENG RUN NO DEFECTS NOTED AT THIS TIME IAW B767 29-11-00, 71-00-00 AMM. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 100,128 hrs · 45,213 cycles

DURING PUSH BACK AUTO THROTTLE DISCONNECT EICAS MESSAGE AND ALL THRUST REFERENCE INDICATIONS DISAPPEARED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE AUTO THROTTLE SYSTEM IAW ABX MEL 22-30-1A, PLACARD INSTALLED AND MX PROCEDURES C/W. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 100,077 hrs · 45,200 cycles

L ENG ANTI-ICE VALVE STUCK CLOSED AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED ENGINE RUN AND LIGHT EXTINGUISHED WHEN THROTTLES ADVANCED IAW 71-00-00-201. AIRCRAFT RETURNED TO SERVICE

Part: CONTROL SYSTEM — CORRODED (LEFT/RIGHT WING) · airframe 99,959 hrs · 45,155 cycles

DURING TAKEOFF FLIGHT CONTROLS BECAME EXTREMELY HEAVY TO OPERATE DECLARED EMERGENCY, RETURNED TO CVG. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LEFT AND RIGHT LCCA OUTPUT QUADRANTS AND RIGHT OUTPUT CONTROL QUADRANT WITH FROZEN BEARINGS. REMOVED AND REPLACED RIGHT LCCA OUTPUT QUADRANT IAW B767 AMM 27-11-78. REPLACED BEARINGS AND REINSTALLED SAME IAW B767 AMM 27-11-34 AND SOPM 20-50-03 .REFERENCE WORK ORDER 2023744 FOR ALL MAINTENANCE ACTIONS. AIRCRAFT RETURNED TO SERVICE AFTER MAINTENANCE EVALUATION FLIGHT.

Part: STRINGER — CORRODED (BS1263-1285 S29L) · corrosion level 2 · airframe 99,858 hrs · 45,124 cycles

DURING ROUTINE LINE MAINTENANCE IN CVG MAINTENANCE DISCOVERED INTERCOSTAL AND STRINGER AT STATION 1263-1285 29L CORRODED. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED CORRODDED STRUCTURE AND INSTALLED NEW INTERCOSTAL AND STRINGER SECTION IAW B767 SRM 51-40-02. AND 53-00-03. FIG. 201. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED · airframe 99,746 hrs · 45,087 cycles

DURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED A CRACK COMMON TO FUSELAGE SKIN P/N 143T3221-2 AT STA 781 AND STR 38L. THE CRACK LENGTH IS 0.5” AND THERE ARE NO REPAIRS IN 767-200 SRM. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. REPAIRED PER ABX-REA-5335-64790-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: SKIN — CRACKED · airframe 99,746 hrs · 45,087 cycles

DURING C CHECK LH O\B ELEVATOR UPPER SURFACE COMPOSITE SKIN CRACKED AT CENTER HINGE ACCESS CUTOUT AT ELEV STA 163.74. SRM 55-20-01 AD1 STATES TO CONTACT BOEING FOR ALLOWABLE DAMAGE LIMITS IN CRITICAL AREA. BOEING WAS CONTACTED THROUGH SERVICE REQUEST 3-5489042895 AND PERMANENT REPAIR INSTRUCTIONS WERE PROVIDED IN PEF-PEF-22-0025-09B REPAIRED PER ABX-REA-5520-64791-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: NONE — NONE · airframe 98,775 hrs · 44,774 cycles

SPD BRAKE KORRY LIGHT FAINTLY ON. NO EICAS MESSAGE UNLESS MASTER DIM/TEST. AIRCRAFT RETURNED TO GATE AND GROUNDED BY MAINTENANCE. FOUND EGPWS STUCK IN TEST MODE. RERACKED M983 AND ACCOMPLISHED LDG AND CONFIG TESTS IAW B767 AMM 31-51-00. SPDBRAKE LIGHT OPS NORMAL. THIS ACTION CLOSES DI. PLACARD REMOVED. NO MAINT REACTIVATION. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 98,317 hrs · 44,621 cycles

AFTER BLOCK OUT LT. GEN. EICAS DISPLAYED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED L/H IENGINE GENERATOR IAW MEL 24-00-1-1 PLACARD INSTALLED AND MAINTENANCE PROCEDURES COMPLIED WITH. MBCB 4/24/2022. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 98,270 hrs · 44,607 cycles

L ENGINE BLEED VALVE EICAS AND L ENG SWITCH LIGHT ON ON TAKEOFF ROLL. LOW SPEED ABORT AT 30-40 KTS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED LH HPSOV IAW MEL 36-11-2-1. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (LT EEC) · airframe 98,102 hrs · 44,554 cycles

LH EEC CIRUIT BREAKER POPPED ON PUSH BACK. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED LH ENG EEC TRIM CONT C/B PER REA ABX-REA-7320-64618-00 AND GMM CHAPTER 01, SECTION 7.04 FOR MAINTENANCE TRACKING. PLACARD INSTALLED. AIRCRADFT RETURNED TO SERVICE.

Part: RELAY — STICKING (MEC) · airframe 97,834 hrs · 44,471 cycles

ADP REMAINS ON IN AUTO MODE, AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERF CONTINUITY CK OF MAIN HYD. SYS CONT PNL PER B767 WDM 29-11-32 CK GOOD PERF B767 FIM 29-11 FT 839. ADP ON DEMAND RELAY (K684) FOUND BAD. REMOVED AND REPLACED PER WDM 29-11-32 & BSWPM 20-81-22. OPS CK GOOD PER AMM 29-11-00. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — CRACKED (ZONE 100) · airframe 97,782 hrs · 44,454 cycles

DURING TAXI OUT CENTER HYDRAULIC QUANTITY DROPPED TO ZERO. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED & REPLACED ACMP PRESSURE/CASE DRAIN FILTER MODULE DUE TO LEAKAGE IAW AMM 29-11-18. LEAK CHECK GOOD. NO LEAKS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 97,555 hrs · 44,375 cycles

ADP PRESSURE LIGHT AND DEMAND PUMP EICAS MESSAGE DISPLAYED WITH DEMAND PUMP SW IN ON POSITION DURING TAXI, AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT ADP IN B767 FIM 29-11 FAULT TREE 814 TO A BAD ADP PRESSURE SWITCH, #32 ON THE FAULT TREE. ADP WAS PLACED ON MEL IAW MEL 29-11-3. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELEMENT — SHORTED (ZONE 500) · airframe 97,525 hrs · 44,364 cycles

DURING CRUISE, EICAS MESSAGE L BLD DUCT LEAK APPEARED AND LEFT DUCT LEAK DISCREET LIGHT ILLUMINATED. QRH PROCEDURES PERFORMED. CREW ELECTED TO DIVERT TO ONT. DUE TO POSSIBLE ICING CONDITIONS AT ORIGINAL DESTINATION. AIRCRAFT GROUNDED BY MAINTENANCE. OPENED ALL UNDER-WING PANEL USING APU AIR, PERFORMED LEAKS CHECKED, NO LEAKS, CONTINUITY CHECK AT D10222 PIN 6 & 9, READING 4.6 OHMS TO GROUND 4M OHMS, USING MEGER METER, LOOPS ARE SHORTENED TO GROUND. CHECKED EACH LOOP, FOUND TSO209 BAD, REPLACED TS0209 WITH POWER ENGINE RUN AND NO DEFECTS NOTED. OPS CHECKED GOOD IAW B767 MM 26-18-00. AIRCRAFT RETURNED TO SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION (ELEVATOR FEEL) · airframe 96,754 hrs · 44,103 cycles

ARRIVED WITH ELEV FEEL EICAS STATUS MESSAGE.PERFORMED FIM 27-31 F/T 806 - MSG CLEARED SYSTEM OK. AFTER BLOCK OUT, AIRCRAFT RETURNED TO BLOCKS WITH AIL LOCKOUT AND RUDDER RATIO EICAS MESSAGES AND THE RIGHT ENGINE #1 IGNITION SYSTEM FAILED. AICRAFT GROUNDED BY MAINTENANCE. RESET CB OPS CHECK GOOD IAW AMM 27-21-00. DEFERRED RH ENGINE #1 IGNITION SYSTEM (MEL 74-00-1B - DI# 25187). AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAULTY (LEFT ENG HI PRES) · airframe 96,708 hrs · 44,085 cycles

LH ENG BLEED VALVE EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.R&R LH HIGH PRESSURE CONTROLLER IAW AMM 36-11-08 LEAK & BITE CHECK GOOD. AICRAFT RELEASED FOR FLIGHT.

Part: MODULE — MALFUNCTIONED (FIRE BELL) · airframe 96,280 hrs · 43,937 cycles

FIRE BELL SOUNDED DURING TAXI OUT AND WILL NOT SILENCE. NO OTHER WARNING LIGHTS ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED MODULE ASSY. AURAL WARNING CARD PER B767 AMM 26-10-01. NO FIRE BELLS SOUNDING. OPS CHECK GOOD AT THIS TIME. AIRCRAFT RELEASED FOR FLIGHT.

Part: STARTER — FAILED (RT ENGINE) · airframe 96,014 hrs · 43,842 cycles

RH ENGINE STARTER FAILED ON ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. STARTER WAS REPLACED IAW AMM 80-11-01 AND AIRCRAFT WAS RELEASED FOR FLIGHT.

Part: STARTER — FAULTY (RT ENGINE) · airframe 95,975 hrs · 43,830 cycles

RH ENG WOULD NOT START. WILLNOT GET ANY ROTATION ,WHEN, "GND " IS SELECTED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. ENGINE STARTER WAS REMOVED AND REPLACED IAW AMM 80-11. AIRCRAFT RELEASED FOR FLIGHT.

Part: FITTING — CORRODED (TAILCONE) · corrosion level 2 · airframe 95,096 hrs · 43,508 cycles

CORROSION IN TENSION FITTING BOLT HOLE ON TAIL CONE LOWER LT HOLE. REMOVED AND REPLACED FITTING P/N 148T9180-3, IAW B767 200 SRM 51-40-02.

Part: COMPUTER — MALFUNCTIONED (YAW DAMPER) · airframe 94,944 hrs · 43,461 cycles

AFTER BLOCK OUT RUDDER RATIO LIGHT AND EICAS MESSAGE BTB AND GROUNDED. PERFORMED RESET ON RRCM, YAW DAMPER COMPUTER, AS PER AMM 27-21-00. OPERATIONS CHECK GOOD. AIRCRAFT RELEASED.

Part: COMPUTER — MALFUNCTIONED (RUDDER RATIO) · airframe 94,986 hrs · 43,457 cycles

AFTER ENGINE START- RUUDER RATIO DISCRETE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND AIRCRAFT GROUNDED. RESET LT &RT RUDDER RATIO COMPUTERS, REF B767 FIM 27-21 FT 804. NO DEFECTS NOTED. AIRCRAFT RELEASED.

Part: WARNING MESSAGE — FALSE ACTIVATION (L1 DOOR) · airframe 94,940 hrs · 43,436 cycles

L1 DOOR INDICATION AFTER PUSH BACK. AIRCRAFT BACK TO GATE AND GROUNDED. OPERATED OUTSIDE DOOR HANDLE AND INSIDE HANDLE VERIFIED L1 DOOR IS CLOSED AND LOCKED. DEFERRED IAW ABX MEL 52-71-1-1. AIRCRAFT RELEASED.

Part: PUMP — SEIZED (HYD SYSTEM) · airframe 94,864 hrs · 43,409 cycles

C HYD DEM PUMP LIGHT ILLUMINATED AFTER FLAPS SELECTED 15A/C BTB AND GROUNDED. REMOVED ADP, IAW B767 AMM 29-11-03. RE-INSTALLED NEW ADP, IAW B767 AMM 29-11-03. A/C RELEASED.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 94,864 hrs · 43,409 cycles

ON TAKE-OFF AFTER GEAR RETRACTION LOST C HYD PRESS. AICRAFT LANDED AND WAS GROUNDED. HYDRAILIC LINE IN WHEEL WELL WAS FOUND CRACKED. LINE WAS REPLACED AND AIRCRAFT WAS PUT BACK IN SERVICE.

Part: BULKHEAD WEB — BUCKLED · airframe 94,597 hrs · 43,280 cycles

HAECO NR-42871 AFT SIDE OF AFT PRESSURE BULKHEAD JUST BELOW TEAR STRAP TS6 AT RADIAL STIFFENER RS17 SKIN BUCKLED AT MULTIPLE RIVET LOCATIONS, REF ABX-REA-5380-64028-00.

Part: STIFFENER — CRACKED (BS 1065) · airframe 94,597 hrs · 43,280 cycles

DURING MAINTENANCE VISIT AT HAECO GSO, PRODUCTION PERSONNEL REPORTED CRACK DAMAGE ON BS 1065 BULKHEAD, STIFFENER NR 6, 145T2668-4, APPROXIMATELY AT BL 0.00. THE CRACK DAMAGE SEVERED THE SUBJECT STIFFENER. THE DAMAGE WAS REMOVED BY TRIMMING THE SECTION OF THE PART, REF.ABX-REA-5350-64020-00.

Part: SKIN — GOUGED (NR 1 STRUT) · airframe 94,597 hrs · 43,280 cycles

AIRCRAFT N744AX IS IN HAECO-GSO FOR MAINTENANCE VISIT. MAINTENANCE REPORTED 2 GOUGE DAMAGES ON NR 1 STRUT, OUTBOARD SKIN (311T1450-3). IDENTIFY AS DAMAGE 1 DAMAGE WAS REMOVED WITH REMAINING MATERIAL OF 0.035 INCHES (56.25%) FROM INITIAL THICKNESS OF 0.080 INCHES. THE B767-200 SRM 54-51-01 ALLOWABLE DAMAGE 1 FIGURE 101, DETAIL III, ALLOWS 10% MATERIAL LOSS. NO PUBLISH REPAIR DOCUMENT IS AVAILABLE FOR THE SUBJECT, REF ABX-REA-5430-64023-00.

Part: RIB — DAMAGED (RT WING TE FLAP) · airframe 94,597 hrs · 43,280 cycles

RT WING OUTBOARD TRAILING EDGE FLAP UPPER SIDE CENTER RIB 4 FOOT 3 INCHES FROM OUTBOARD END, HAS DRILL DAMAGE AT FASTENER HOLE, REF ABX-REA-5750-64022.

Part: FLOORBEAM — CORRODED (BS 1417) · airframe 94,597 hrs · 43,280 cycles

DURING MAINTENANCE VISIT, CORROSION DAMAGE WAS NOTED TO THE LOWER AFT SURFACE OF THE STA 1417 FLOOR BEAM UPPER (368-53-16-94201-101) T-CAP FLANGE, AT LBL 6, THAT FALLS OUTSIDE OF THE LIMITS OF IAI SRM SUPPLEMENT 53-00-51. THE CORROSION DAMAGE IS LOCATED IN THE TAPERED END SECTION OF THE UPPER FLANGE WITH THE GREATEST MEASURED MATERIAL LOSS BEING 46.5 PERCENT. THE REPAIR ACCOMPLISHED IS ACCEPTABLE AND HAS STAGE 1 APPROVAL FOR STATIC STRENGTH, PER FAA FORM 8110-3 SIGNED BY ROBERT MANASHI, DERT-710167-SW, DATED 10-SEP-2020. REF.ABX-REA-5360-64021-00.

Part: DOOR FRAME — DAMAGED (BS 492) · airframe 94,597 hrs · 43,280 cycles

DURING MAINTENANCE VISIT AT HAECO GSO, PRODUCTION PERSONNEL REPORTED DAMAGE ON THE MAIN CARGO DOOR OPENING FORWARD FRAME STA 492 BETWEEN S-7L AND S-8L. DAMAGES ARE MINOR, HOWEVER, IAI B767 SRM SUPPLEMENT NOTES TO CONTACT IAI FOR ALLOWABLE DAMAGE LIMITS. THE DAMAGE IS LOCALIZED ON THE FRAMES INNER AFT CORNER EDGE WITH A LENGTH OF 1.10-INCH, A WIDTH OF 0.005-INCH, AND A MAX CORNER DEPTH OF 0.012-INCH. CUSTOMER REPORTED TO IAI THAT DAMAGE WAS CAUSED TO BOTH MDCD SURROUND MAIN FRAMES AT STA 492 AND STA 632. SEE PAGES FROM 3 TO 5 FOR VIEWS OF DAMAGE. DAMAGES WERE REMOVED PER 767-200 SRM 51-10-02. SEE PAGES 4 AND 5 FOR VIEWS OF DAMAGE REMOVED. SURFACE HFEC INSPECTION WAS PERFORMED IN REGION AROUND DAMAGE LOCATION WITH NO DEFECTS FOUND, REF.ABX-REA-5333-64025-00.

Part: DOOR FRAME — DAMAGED (BS 632) · airframe 94,597 hrs · 43,280 cycles

DURING MAINTENANCE VISIT AT HAECO GSO, PRODUCTION PERSONNEL REPORTED DAMAGE ON THE MAIN CARGO DOOR OPENING AFT FRAME STA 632 BETWEEN S-6L AND S-8L. DAMAGES ARE MINOR, HOWEVER, IAI B767 SRM SUPPLEMENT NOTES TO CONTACT IAI FOR ALLOWABLE DAMAGE LIMITS. THE DAMAGE IS LOCALIZED ON THE FRAMES INNER AFT CORNER EDGE AT TWO LOCATIONS, DAMAGE 1 WITH A LENGTH OF 2.20-INCH, A WIDTH OF 0.150-INCH, AND A MAX CORNER DEPTH OF 0.020-INCH, AND DAMAGE 2 WITH A LENGTH OF 1.20-INCH, A WIDTH OF 0.050-INCH, AND A MAX CORNER DEPTH OF 0.010-INCH. DAMAGES WERE REMOVED, PER 767-200 SRM 51-10-02. SEE PAGES 4 AND 5 FOR VIEWS OF DAMAGE REMOVED, REF.ABX-REA-5333-64026-00.

Part: DISPLAY — MALFUNCTIONED (EICAS) · airframe 64,284 hrs · 43,882 cycles

LOWER EICAS SCREEN WOULD NOT DISPLAY THE FLIGHT CONTROL PAGE. AIRCRAFT WAS GROUNDED.

Part: WARNING MESSAGE — ACTIVATED · airframe 94,379 hrs · 43,177 cycles

MASTER WARNING WITH GEAR NOT DOWN EICAS. EICAS CONFIG LIGHT WHILE TAXIING AND STOPPED. IT OCCURRED OVER A DOZEN TIMES. THE AIRPLANE WAS GROUNDED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 93,975 hrs · 43,000 cycles

R AOA PROBE HEAT EICAS MESSAGE SHOWS R AOA LIGHT IS ON. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,467 hrs · 41,954 cycles

CRACK IN FUSELAGE SKIN AT BODY STATION 760, STRINGER 35R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,467 hrs · 41,954 cycles

CORROSION ON KEELBEAM AT BODY STATION 975, LBL 11. THE KEELBEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 91,467 hrs · 41,954 cycles

CORROSION ON THE AFT DOOR JAMB FRAME OF THE FORWARD LOWER CARGO DOOR. THE FRAME WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 91,467 hrs · 41,954 cycles

DAMAGE IN FUSELAGE SKIN DOUBLER AT BODY STATION 399. THE DOUBLER WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (LT WING) · airframe 91,467 hrs · 41,954 cycles

CORROSION ON LEFT WING REAR SPAR TO UPPER TRAILING EDGE ATTACH CHORD AT WING STATION 284. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,467 hrs · 41,954 cycles

CORROSION ON THE HORIZONTAL KEELBEAM WEB FROM BODY STATION 964 TO 968 AND LBL 8 TO RBL 8. THE KEELBEAM WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: WEB — CORRODED (RT WING) · airframe 91,467 hrs · 41,954 cycles

CORROSION ON WEB OF THE RIGHT WING LEADING EDGE AT LEADING EDGE STATION 630. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: RIB — GOUGED (TE FLAP) · airframe 91,467 hrs · 41,954 cycles

GOUGE ON THE INTERNAL SPICE RIB OF THE LEFT OUTBOARD FLAP AT OTEF STATION 83.73. THE RIB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,467 hrs · 41,954 cycles

CORROSION ON THE LEFT OUTER KEELBEAM A-FRAME CHORD AT BODY STATION 977. THE KEELBEAM A-FRAME CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,467 hrs · 41,954 cycles

CRACK IN FUSELAGE SKIN AT BODY STATION 1654, STRINGER 13L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 91,467 hrs · 41,954 cycles

CORROSION ON THE FORWARD DOOR JAMB FRAME OF THE FORWARD LOWER CARGO DOOR. THE FRAME WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,467 hrs · 41,954 cycles

CORROSION ON CENTER RIB OF THE BULK CARGO DOOR LOWER SILL. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

CORROSION ON HORIZONTAL STABILIZER CENTER BOX, OUTBOARD SIDE OF RIB 2R LOWER STRINGER 3 VERTICAL LEG AFT SIDE. FOUND BEYOND LIMITS, REMOVED 72 INCHES OF STRINGER 3, FABRICATED AND INSTALLED IAW REA B655-62257-MR AND SRM 51-40-02. AIRCRAFT WAS GROUNDED.

Part: ANGLE — CORRODED (BS 1725-1758) · airframe 88,120 hrs · 40,654 cycles

BS 1726 - 1731, STRINGER 4R APU INLET DUCT RETAINER CORRODED AROUND NUT PLATES. REMOVED AND REPLACED APU INLET DUCT RETAINER ANGLE IAW SRM 51-40-02 PAR 4, 7 AND DRAWING 148T3120.

Part: SUPPORT ANGLE — CORRODED (BS 1725-1767) · airframe 88,120 hrs · 40,654 cycles

UPPER ATTACH STRUCTURE CORRODED UNDER APU INTAKE DOOR. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II. FABRICATED A NEW ATTACH STRUCTURE IAW DRAWING 148T3120, AND INSTALLED IAW DRAWING 148T3210, AND SRM 51-40-02 PAR 4,7. AIRCRAFT GROUNDED.

Part: SKIN — CORRODED (APU DOOR) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

LEFT APU DOOR INNER SKIN CORRODED JUST AFT OF 5TH FRAME FROM FORWARD END. REPAIRED IAW SRM 52-40-01 FIG 201 REPAIR 5. AIRCRAFT GROUNDED.

Part: KEELBEAM — CORRODED (BS 990-1000) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

CORROSION ON KEEL BEAM LOWER CHORD APPROXIMATE BS 990-996, LBL9 ACCESSED BETWEEN MAIN LANDING GEAR DOORS. REPAIRED LOWER KEEL BEAM CHORD AT STATION 990-996 LBL9 IN ACCORDANCE WITH REA- B653-62220-MR. ACFT GROUNDED.

Part: ANGLE — CORRODED (KEEL BEAM) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

CORROSION ON KEEL BEAM LOWER ANGLE BS 1002 - 1015, LBL 9. REPAIRED IAW REA-B653-622220-MR. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (BS 956-973) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

THREE AREAS OF CORROSION ON KEEL BEAM LOWER CHORD (TOP AND BOTTOM) APPROXIMATE STATION 956-970, LBL9 ACCESSED BETWEEN MAIN LANDING GEAR DOORS. REPAIRED LOWER KEEL BEAM AT STATION 956-970 LBL9 IN ACCORDANCE REA-B653-62220-MR. ACFT GROUNDED.

Part: ANGLE — CORRODED (KEEL BEAM) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

CORROSION ON KEEL BEAM LOWER ANGLE BS 1025 - 1030, LBL 9. REPAIRED IAW REA B653-62220-MR. AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (BS 883) · airframe 88,120 hrs · 40,654 cycles

BS 883.5 LBL 89, SIDE FRAME AT LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA 53000049-101 AND REA B653-62233-SB. AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (BS 859) · airframe 88,120 hrs · 40,654 cycles

BS 859.5 LBL 89, SIDE FRAME AT LOWER TRANSITION RADII CRACKED (BELOW FLOOR LINE). REF: J/C NEA 53000045-001 ES02570 PG 2 AIRCRAFT WAS GROUNDED.

Part: ANGLE — CRACKED (ZONE 400) · airframe 88,120 hrs · 40,654 cycles

ANGLE CRACKED ON OUTBOARD PYLON JUST ABOVE AND FORWARD OF STRUT ACCESS DOOR. REMOVED AND REPLACED THE ANGLE IAW DRAWING 313T3310 AND SRM 51-40-02 PAR 7.

Part: RIB — CRACKED (LT WING SLAT) · airframe 88,120 hrs · 40,654 cycles

NR 4 SLAT INBOARD DRIVE ROD CUTOUT, INBOARD NOSE RIB CRACKED. REMOVED AND REPLACED INBOARD NOSE RIB ON NR 4 SLAT IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.

Part: ANGLE — CRACKED (BS 1638 FRAME) · airframe 88,120 hrs · 40,654 cycles

BS 1678 STRINGER 3R FRAME ANGLE CRACKED. REMOVED AND REPLACED FRAME ANGLE IAW SRM 51-40-07. AIRCRAFT WAS GROUNDED.

Part: ANGLE — CRACKED (BS 1702) · airframe 88,120 hrs · 40,654 cycles

BS 1702 STRINGER 3R FRAME ANGLE CRACKED. REMOVED AND REPLACED FRAME ANGLE IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (BS 883) · airframe 88,120 hrs · 40,654 cycles

BS 883.5 RBL 89, SIDE FRAME AT LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA53000050-101. AIRCRAFT WAS GROUNDED.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

LEFT WING LEADING EDGE BS 698 FORWARD LOWER PANEL ATTACH NUT PLATE STRIP CORRODED. NOSE BEAM AT NUT PLATE LOCATIONS WAS FOUND CORRODED BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED NOSE BEAM WEB AND FABRICATED REPLACEMENT NOSE BEAM WEB FROM 7075T-6 .050 PO# 008909 IN ACCORDANCE WITH BOEING DRAWING 114T2300 AND 767 SRM 51-30-01. INSTALLED REPLACEMENT -189 NOSE BEAM IN ACCORDANCE WITH 767 SRM 51-40-02 PAR 4,7,9. SDR INFO: CORRODED, LEVEL: 2, PART NUMBER: 114T2300-189, PART NAME: NOSE BEAM WEB, LOC: LES 698 TO LES 708. AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (BS 859) · airframe 88,120 hrs · 40,654 cycles

BS 859.5 RBL 89, SIDE FRAME LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA 53000048-101. AIRCRAFT WAS GROUNDED.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,120 hrs · 40,654 cycles

CORROSION ON SUPPORT ANGLE AT THE AFT LEFT CORNER OF THE INNER KEEL BEAM AREA ACCESSED THRU PANEL 139FZ. REMOVED CORROSION ON SUPPORT ANGLE WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-50-12 FIGURE 101 DETAIL II AND TALE I. REMOVED .010 OF MATERIAL, ORIGINAL THICKNESS .160. TREATED AND PRIMED AREA IN ACCORDANCE WITH AMM 51-21-04, 51-21-10. AIRCRAFT WAS GROUNDED.

Part: TORQUE TUBE — CRACKED (NR 3 SPOILER) · airframe 87,136 hrs · 40,284 cycles

DURING PREPARATION OF FLAP REMOVAL, WHILE INSTALLING NR 3 SPOILER LOCK, FOUND ACTUATOR TO WING OTBD ATTACH LUG BROKEN OFF & INBD LUG BADLY WORN. R & R NR 3 SPOILER ACTUATOR TORQUE TUBE IAW AMM 27-61-01, & 27-61-02. SDR CRACK 3 INCHES, PN 1134T1440-1, SN NSN, PART NAME SPOILER TORQUE TUBE ASSEMBLY, LOCATION: WS 657 LT TO WS 657 LT. ACFT WAS GNDED.

Part: WEB — CRACKED (LT NACELLE) · airframe 86,190 hrs · 39,535 cycles

STRUCTURAL WEB IS CRACKED AT THE FWD MOST NOSE COWL ANTI-ICE DUCT SUPPORT ROD BRACKET. REMOVED DAMAGED WEB, FABRICATED & INSTALLED NEW WEB IAW SRM 51-40-02 & DWG 311T1510. CRACKED 3.2 INCHES, PN 311T1510-59, SN N/A, PART NAME WEB, FS & BS LOCATION ON ACFT NAC WL 150, STRINGER WS LOCATION ON ACFT WS 166 TO WS 169.8. ACFT WAS GNDED.

Part: SUPPORT — DAMAGED (RT WING) · airframe 86,190 hrs · 39,535 cycles

FASTENER HOLE ON NR 1 SUPPORT 1, 2, 3 BEAM RT SIDE FWD OF NR 2 JOINT UPPER HOLE HAS DAMAGE IN HOLE. REAMED HOLE & INSTALLED OVERSIZED FASTENER IAW REA-C027-61321-MR. HOLE DAMAGE, PART NR 113T1313-7, PART NAME FLAP SUPPORT, 1 - 3 BEAM, EXACT LOCATION 800, SN ABXT803. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 86,190 hrs · 39,535 cycles

RIGHT WING NR 8 FLAP SUPPORT MECHANISM 1, 2, 3 BEAM INBD STUD HOLE HAS HFEC DEFECT INDICATION. CORROSION VISIBLE. NR 8 SUPPORT 1, 2, 3 BEAM REROUTED TO COMPONENT REPAIR SHOP FOR REPAIR IAW CMM IAW REA C057-61312-MR. CORRODED LEVEL 2, PART NR 113T1313-8, PART NAME NR 8 SUPPORT ASSEMBLY 1 - 3, SN A4683, EXACT STRINGER WS LOCATION ON ACFT FROM 798.2 TO 798.3. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 86,190 hrs · 39,535 cycles

RIGHT WING NR 7 FLAP SUPPORT 1,2, 3 BEAM HAS HFEC DEFECT INDICATION IN OTBD STUD HOLE. NR 7 SUPPORT 1, 2, 3 BEAM REROUTED TO COMPONENT REPAIR SHOP FOR REPAIR IAW CMM IAW REA C057-61311-MR. CORRODED LEVEL 2, PART NR 113T1314-16, PART NAME NR 7 SUPPORT 1 - 3 ASSEMBLY, SN A4683, EXACT STRINGER WS FROM 612.2 TO 612.3. ACFT WAS GNDED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 86,190 hrs · 39,535 cycles

TOOLING MARKS ON REPAIR DOUBLER AT STATION 1373 IN BETWEEN STRINGER 29R & 30R. R & R DOUBLERS IAW ERA 379839-14. FABRICATED DOUBLERS FROM 2024-T3 .100 IAW ERA 379839-14. REPLACED DOUBLERS BECAUSE OF TOOLING MARKS ON LOWER DOUBLER. TOOLING MARKS, PN 146T3531-2, SN NSN, PART NAME SKIN, FS & BS LOCATION ON ACFT FS 1361 TO 1381, STRINGER LOCATION ON ACFT STRINGER 28R TO 29R. ACFT WAS GNDED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,190 hrs · 39,535 cycles

CRACKED SUPPORT ANGLE AT AFT END OF FORE TO AFT LOWER BEAM AT REAR SPAR APPROX RBL 42. FABRICATED NEW SUPPORT ANGLE FROM 2075-0-090 PO 0055105. HEAT TREATED TO 2075-T6 IAW DWG 111T1000. CRACKED 4.7 INCHES, PN 111T1000, PART NAME ANGLE, SN NSN, FS & BS LOCATION 970 TO 975, STRINGER & WS LOCATION RBL 42 TO RBL 42. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 86,190 hrs · 39,535 cycles

PANEL 552CB AFT ATTACH CHORD SPLIT ON EDGE. R & R CHORD. REINSTALLED PANEL 552EB & 551YBX IAW SRM 51-40-02. CORRODED L2, PN 654T0391-35, SN NSN, PART NAME CHORD, STRINGER & WS 180 TO 314. ACFT WAS GNDED.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,190 hrs · 39,535 cycles

PANEL ATTACH CROSS MEMBER AT STATION 968 CORRODED AROUND NUTPLATE ON LT SIDE. R & R ATTACH CROSS MEMBER AT STATION 968 IAW SRM 51-40-08, 51-40-05 & 51-40-02. PN 145T8629-3, PART NAME CROSS MEMBER, SN NSN, CORRODED L2, EXACT FS LOCATION ON ACFT 968 TO 968 LOWER FUSELAGE STATION. ACFT WAS GNDED.

Part: FITTING — CRACKED (L1 DOOR) · airframe 84,755 hrs · 38,567 cycles

L1 DOOR HAS A POSSIBLE CRACK ON THE LOWER FRONT AND AFT FITTINGS OF THE DOOR, IN THE BACK POCKET OF THE FITTINGS. INSTALLED NEW LOWER BEAM IAW B767 SRM 51-40-02 AND DWG 141T6109, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

LEFT SIDE SKIN UNDER FAILSAFE CUTOUT SHOWS SIGNS OF CORROSION. REPAIRED AREA, ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

STA 955 S22L FAILSAFE CUTOUT CENTER HOLE SHOWS CRACK INDICATION. REAMED HOLE IAW B767-200 SRM 51-10-02. NDT VERIFIED. NO DEFECTS, INSTALLED 2ND OVERSIZE FASTENER IAW AMES DOCUMENT 47043REA02, ACFT WAS GROUNDED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

RIGHT SIDE FAILSAFE STRAP FOUND WITH .50" CRACK RADIATING FROM LOWER HOLE AT APPROX 9 O'CLOCK POSITION. FRETTING CORROSION ON OPPOSITE SIDE OF FITTING WILL BE CLEANED UP BY TRIM OUT PROCEDURE. TRIM OUT OF FAILSAFE AND CORRECTIVE ACTION ACCOMPLISHED, ACFT WAS GROUNDED.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

STA 955 LEFT FAILSAFE, INBOARD SIDE, CORROSION AT TEE FITTING REMOVAL LOCATION. FAILSAFE TRIM OUT ACCOMPLISHED ON DOCUMENT 470080RD03, ACFT WAS GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

AT STA 955 LEFT TEE FITTING COMMON TO THE FAILSAFE STAP IS CORRODED. DRILLED NEW TEE FITTING IAW B767 SRM 51-40-05 TEE FITTING INSTALLED ON DOCUMENT 47008ORD03 STEP 15, ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

LEFT FAILSAFE INBD, CRACKED AT CENTER HOLE TEE FITTING REMOVAL LOCATION, CORRECTIVE ACTION (FAILSAFE TRIMOUT) ACCOMPLISHED ON AMES DOCUMENT 470080RD03. ACFT WAS GROUNDED.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

AT STA 955 RIGHT RIGHT SIDE TEE FITTING COMMON TO FAILSAFE, FWD LOWER HOLE OUT BOARD SURFACE CORRODED. DRILLED NEW TEE-FITTING IAW B767 SRM 51-40-05. TEE-FITTING INSTALLED ON DOCUMENT 47008ORD04, ACFT WAS GROUNDED.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,755 hrs · 38,567 cycles

RIGHT WING LEADING EDGE ATTACHING FLANGE (DOUBLER) CRACKED FOR WING TIP FAIRING. REMOVED AND REPLACED RIGHT SIDE WING TIP FWD ATTACH DOUBLER P/N 112T5360-44 USING 2024T3 .063" THICK IAW BOEING DWG 112T5360 AND B767-200 SRM 51-40-02, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 84,755 hrs · 38,567 cycles

HORIZONTAL CENTER SECTION LOWER SKIN BETWEEN S-9 AND S-10 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R-3R. BLENDED AREA ON LOWER SKIN BETWEEN S9 & S10 IAW B767 SRM 55-10-01. FOUND TO BE WITHIN LIMITS IAW REA B655-60486-MR, AIRCRAFT WAS GROUNDED.

Part: SILL — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

UNDER BULK CARGO DOOR SILL LOWER SILL FS 1407-1480 BELOW S32L HAS THE UPPER CHORD OF THE SILL FRAME CORRODED (METAL WAS EXFOLIATED). REMOVED AND REPLACED BULK CARGO DOOR UPPER CHORD OF FLOOR FRAME WITH SERVICEABLE UNIT IAW BOEING SRM 51-40-02 AT FS 1407-1480 S32L NO CRACKS NOTED, ACFT WAS GROUNDED.

Part: FASTENER — CORRODED (HORIZ STAB) · airframe 84,755 hrs · 38,567 cycles

HORIZONTAL BOX, AT S11 UPPER FWD BETWEEN RIB 2-R AND RIB -1-R BRACKET HAVE HARDWARE CORR. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE A PERMANENT REPAIR IAW REA B655-60485-MR. REMOVED ADN REPLACED CORRODED HARDWARE IAW B767-200 SRM 51-40-02 AT S11R RBL 20.5 TO RBL 23.5 LENGTH 3" X 1.25", ACFT WAS GROUNDED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 84,755 hrs · 38,567 cycles

HORIZONTAL CENTER SECTION UPPER S-7 VERTICAL LEG HAS HEAVY CORROSION JUST OUTBOARD OF RIB 1L. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE PERMANENT REPAIR IAW REA B655-60485-MR, ACFT WAS GROUNDED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

CORROSION ANGLE UNDER BULK CARGO DOOR SILL AT FWD EDGE AT STA 1417. REMOVED AND REPLACED NEW ANGLE UNDER BULK CARGO DOOR SILL IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 84,755 hrs · 38,567 cycles

HORIZONTAL CENTER SECTION LOWER RBL 41.5 STR 5 BETWEEN RIBS 2 & 3 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R. CORRODED AREA FOUND TO BE OUT OF LIMITS, REPAIRED AREA IAW REA B655-60481-MR, ACFT WAS GROUNDED.

Part: SLAT — CORRODED (RT WING) · airframe 84,755 hrs · 38,567 cycles

NR 8 SLAT NEEDS REMOVED AND REPLACED DUE TO CORROSION FINDING. REMOVED & REPLACED NR 8 SLAT IAW B767 AMM 27-81-02, ACFT WAS GROUNDED.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

MAIN CARGO DOOR SURROUND CIRCUMFERENTIAL SPLICE SKIN STA 434 CRACKED AT FASTENER FWD 2ND ROW 2" LEFT OF STRINGER 1R LEFAIVE 350125. REPAIRED AREA AT STA 434 UPPER SKIN SPLICE IAW B653-60479-MR. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · airframe 84,755 hrs · 38,567 cycles

RIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 433 APROX FORWARD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.

Part: SPAR — CORRODED (RT WING) · airframe 84,755 hrs · 38,567 cycles

CORROSION ON RIGHT WING UPPER SURFACE FORWARD SPAR ATTACH AREA. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

INTERCOSTAL BEHIND LOWER CARGO DOOR AFT HINGE IS CORRODED. BLENDED AREA, .040" MATERIAL REMAINED FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED INTERCOSTAL, ALL WORK DONE IAW B767 SRM 53-00-04, 51-40-02 PARA 7 & BOEING DWG 435T535-8, ACFT WAS GROUNDED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 84,755 hrs · 38,567 cycles

INTERCOSTAL CRACKED AND CORRODED RIGHT SIDE OF LOWER CARGO FLOOR BETWEEN STA 1263 AND STA 1285. REMOVED AND REPLACED LOWER CARGO FLOOR INTERCOSTAL ON RIGHT SIDE STA 1263 AND STA 1285 IAW B767 SRM 51-40-02 STEP 7(D), ACFT WAS GROUNDED.

Part: SUPPORT BEAM — CORRODED (RT WING) · airframe 84,755 hrs · 38,567 cycles

RIGHT WING AFT OF REAR SPAR WING STATION 360 HAS CORROSION ON SUPPORT BEAM BELOW ANGLE DRIVE FLAP GEARBOX FOR INBD FLAP. REMOVED AND REPLACED CORRODED BEAM IAW B767 SRM 51-40-02. RIGHT WING TRAILING EDGE WS 375 FUSELAGE STA 1043, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · airframe 84,755 hrs · 38,567 cycles

RIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 490 APROX FWD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.

Part: SOCKET — DIRTY (EXTERIOR) · airframe 84,303 hrs · 38,372 cycles

L1 EXTERIOR EMERGENCY LIGHT FAIL TO TEST. REMOVED EXT EMERGENCY LIGHT, AND CLEANED LAMP HOLDER SOCKET PER AMM 33-51-16-2. OPERATIONAL CHECK OK, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S21L IS CRACKED JUST AFT OF STA 676. REMOVED STRINGER SECTION. FABRICATED AND INSTALLED STRINGER S21L IAW REA B653-59503-MR REV IR, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S23L IS CRACKED JUST AFT OF STA 676. REMOVED FABRICATED AND INSTALLED STRINGER S23L IAW REA B653-59505-MR REV IR 10-5-2011, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S25L IS CRACKED JUST AFT OF STA 676. REMOVED FABRICATED AND INSTALLED STRINGER S25L IAW REA B653-59507-MR, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S24L IS CRACKED JUST AFT OF STA 676. REPAIRED DAMAGED SECTION OF STRINGER S24L AT STA 676 PER REA NO B653-59506 MR & IAW B767 SRM 53-00-03 REPAIR 2, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S22L IS CRACKED JUST AFT OF STA 676. REMOVED FABRICATED AND INSTALLED STRINGER 22L IAW REA B653-59504-MR REV IR 10-5-2011, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S10L IS CRACKED JUST AFT OF STA 676. REMOVED STRINGER SECTION, FABRICATED AND INSTALLED STRINGER SECTION AT S10L STA 676 IAW REA B653-59500-MR AND SRM 53-00-03 REPAIR 1, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S7L IS CRACKED JUST AFT OF STA 676. REMOVED STRINGER SECTION, FABRICATED REPAIR FOR S7L STA 676 AND SPLICED IN REPLACEMENT SECTION IAW B767 200 SRM 53-00-03 FIG 201 REPAIR 1 AND REA B653-59499 MR, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S12L CRACKED JUST AFT OF STA 676. REMOVED STRINGER SECTION. FABRICATED AND INSTALLED STRINGER SECTION AT S12L STA 676 IAW REA NR B653-59501-MR & SRM 53-00-03 REPAIR 1, AWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,261 hrs · 37,820 cycles

STRINGER S18L IS CRACKED JUST AFT OF STA 676. REMOVED STRINGER, FABRICATED AND INSTALLED STRINGER SECTION IAW REA B653-59502-MR & SRM 53-00-03 REPAIR 1, AWG.

Part: PANEL — DEFECTIVE (CABIN) · airframe 82,943 hrs · 37,687 cycles

EMERGENCY LIGHT SWITCH NOT FUNCTIONING PROPERLY. WHEN GUARD PLACED INTO COVERED DOWN POSITION, EMERGENCY SWITCH IS MOVED TO "OFF" POSITION. REMOVED AND REPLACED EMERGENCY LIGHT/O2 PANEL ASSY. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO DOOR) · airframe 80,293 hrs · 36,704 cycles

MAIN CARGO DOOR LIGHT ILLUMINATED ON DESCENT. LOADMASTER VISUALLY VERIFIED CARGO DOOR WAS CLOSED AND LATCHED. LIGHT EXTINGUISHED AT APPROX 2.0 PSI CABIN DIFF PRESSURE. DEFERRED MAIN CARGO DOOR INDICATION PER MEL 52-71-1-2. PLACARD INSTALLED MPM 52-11-1 C/W. VERIFICATION OF MAIN CARGO DOOR CLOSED AND LOCKED MUST BE C/W PRIOR TO EACH DEPARTURE.

Part: WARNING SYSTEM — FAULTY (CARGO DOOR) · airframe 79,885 hrs · 36,597 cycles

SHORTLY PRIOR TO TOP OF DESCENT MAIN CARGO DOOR LIGHT ILLUMINATED AND MASTER WARNING LIGHT EXTINGUISHED AT APPROXIMATELY 7000FT. VISUALLY INSPECTED DOOR HOOK AND LATCH AND DOOR HINGES, NO DEFECT NOTED. DEFERRED MAIN CARGO DOOR INDICATION IAW MEL 52-71-1-2. DOOR MUST BE VERIFIED CLOSED LATCHED AND LOCKED BEFORE EACH DEPARTURE. PLACARD INSTALLED MPM 52-71-1.

Part: SUPPORT BEAM — CRACKED (NR 2 NACELLE) · airframe 79,356 hrs · 36,367 cycles

NR 2 INBOARD STRUT INSIDE HYD BAY FWD END HAS A CRACK AT THE TOOLING HOLE AT APPROX NACELLE STA 308.5. INSTALLED REPAIR SPLICE INSIDE HYD BAY ON DOOR LATCH SUPPORT BEAM IAW REA B-58633MR. CRACK LENGTH .25 INCH.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,356 hrs · 36,367 cycles

SEVEN (7) INCH CRACK BETWEEN BODY STA 1725 AND 1746 RT IN SKIN AT STAB CUTOUT. REPAIRED IAW 767 SRM 53-80-01 AND REA B655-58621.

Part: PANEL — CRACKED (LT WING) · airframe 79,356 hrs · 36,367 cycles

PANEL 551TB OUTBOARD OF LT MLG CORNER IS CRACKED. REMOVED AND RE-INSTALLED PANEL 551TB IAW B767 SRM 51-40-02. P/N 113T1615-25, .5 CRACK LENGTH.

Part: SLAT — CRACKED (WING) · airframe 79,356 hrs · 36,367 cycles

NR 12 SLAT LOWER L/E IS CRACKED AT I/B END. REMOVED NR 12 SLAT FOR REPAIR AND RE-INSTALLED IAW BOEING 767 AMM 27-81-02. SLAT REPAIRED IAW BOEING 767 SRM REV 101.

Part: SUPPORT ANGLE — DAMAGED (NR 2 PYLON) · airframe 79,356 hrs · 36,367 cycles

NR 2 PYLON AFT LOWER CANOE I/B AND O/B SUPPORT ANGLES ARE BENT AND CRACKED. REMOVED AND REPLACED I/B AND O/B SUPPORT ANGLE IAW 767 SRM 51-70-11, .5 INCH CRACK LENGTH. P/N 313T1380-12 AND -14.

Part: PANEL — CRACKED (NR 2 NACELLE) · airframe 79,356 hrs · 36,367 cycles

NR 2 ENGINE STRUT OUTBOARD PANEL NR 447ERX IS CRACKED. PANEL REPAIRED ON FORM R-212. P/N 313T1381-52 .75 CRACK LENGTH.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,356 hrs · 36,367 cycles

BELOW THE FWD LOWER CORNER OF THE APU INTAKE DOOR AT FS 1725 & STRINGER 7R THERE ARE TWO CRACKED FASTENERS AND TWO FUSELAGE SKIN CRACKS. CRACKS MEASURE 1.156 AND 1.0 IN LENGTH. REPAIRED SKIN IAW B767-200 SRM 53-80-01.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 79,356 hrs · 36,367 cycles

NR 2 PYLON STRUCTURE IS CRACKED AT NOSE COWL ANTI ICE DUCT BRACKET AT THE FWD END OF PYLON. REMOVED AND REPLACED DAMAGED WEB AND BRACKET IAW B767-200 SRM 51-40-02, 1.5 CRACK LENGTH.

Part: ATTACH ANGLE — CRACKED (NR 1 PYLON) · airframe 79,356 hrs · 36,367 cycles

NR 1 PYLON ATTACH ANGLE IS CRACKED O/B SIDE AFT OF O/B COWLS AFT HINGE FITTING AT STA NAC318. REMOVED NR 1 ENG EXHAUST SLEEVE IAW B767 MM 78-11-01. REPAIRED ATTACH ANGLE IAW B767 MM 51-40-02 & DRAWING 313T1380. RE-INSTALLED NR 1 EXHAUST SLEEVE IAW B767 MM 78-11-01, 1.0 INCH CRACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,356 hrs · 36,367 cycles

RT FUSELAGE AROUND STA 1660 JUST ABOVE THE HORIZONTAL STABILIZER LEADING EDGE THERE IS BUBBLED UP PAINT WITH BARE METAL EXPOSED WITH POSSIBLE CRACK INDICATION ON THE SKIN. REPAIRED CRACKED AREA ON RT FUSELAGE AROUND STA 1660. P/N 148T3131-4, 1.0 CRACK LENGTH.

Part: WIRE HARNESS — DAMAGED (CARGO BAY) · airframe 79,311 hrs · 36,346 cycles

EICAS MESSAGE APU BLEED VALVE DISPLAYED. APU BLEED VALVE LIGHT ILLUMINATED. DUCT PRESS NORMAL. STATUS MESSAGE AFT EQ EXH FAN 1. FOUND WIRE HARNESS IN NR 3 PIT AREA DAMAGED. WIRE BUNDLE IN AFT CARGO DOOR CEILING AREA OVERHEATED & HAS MULTIPLE WIRES DAMAGED. IN WORK AT THIS TIME.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 77,551 hrs · 35,867 cycles

CLIMBING OUT OF KIX AT FL340, THE RIGHT ENGINE COMPRESSOR STALLED 3 TIMES, PULLED BACK THE RIGHT THROTTLE JUST A LITTLE AND THE STALLS STOPPED. THE ANTI-ICE WAS OFF, A/T WERE ON. AIRCRAFT CONTINUED TO CLIMB AND THERE WERE NO POWER CHANGES. THERE WERE NO ABNORMAL ENGINE INDICATIONS. CREW PERFORMED AN AIR TURNBACK AND LANDED AT KIX WITH NO FURTHER INCIDENT. REPLACED THE RIGHT ENGINE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 75,510 hrs · 35,189 cycles

EMERGENCY LIGHTS BATTERY PACK M735 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM N739AX, INSTALLED IN 744AX IAW B767 MM 33-51-07. OPS CHECK GOOD. (S)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY PACK M734 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M734 IAW MM 33-51-07. OPS CHECKED GOOD. (K)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 75,510 hrs · 35,189 cycles

EMERGENCY LIGHT BATTERY PACK M737 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM 739AX , INSTALLED IN 744AX IAW B767 M 33-51-07. OPS CHECKED GOOD. (S)

Part: MEC — DEFECTIVE (RT ENGINE) · airframe 74,964 hrs · 35,029 cycles

RT ENG COMPRESSOR STALL ON CLIMBOUT. PERFORMED CALLED FOR ITEMS. ENG RESPONDED OK AT 80-85% N1 BUT STALLED AGAIN AT CLIMB POWER. REMOVED AND REPLACED NR 2 ENG MEC IAW B767 MM 73-21-07-4. TESTED MEC IAW B767 MM 71-00-00. NR 2 ENG COMPRESSOR STALL AT 84%. (S)

Part: OVEN — SHORTED (GALLEY) · airframe 74,266 hrs · 34,822 cycles

MICROWAVE SHORTED OUT WHEN IN USE. TOP RIGHT BACK SIDE SPARKED AND FIRE CAME OUT. CIRCUIT BREAKERS PULLED FOR GALLEY. REMOVED AND REPLACED MICROWAVE. OPS CHECKED GOOD IAW B767 MM 25-31-00.

Part: OVEN — SHORTED (GALLEY) · airframe 74,266 hrs · 34,822 cycles

MICROWAVE SHORTED OUT WHEN IN USE. TOP RIGHT BACK SIDE SPARKED AND FIRE CAME OUT. CIRCUIT BREAKERS PULLED FOR GALLEY. REMOVED AND REPLACED MICROWAVE. OPS CHECKED GOOD IAW B767 MM 25-31-00.

Part: FMC — DEFECTIVE (E/E BAY) · airframe 73,587 hrs · 34,629 cycles

AFTER LIFT OFF AT KIX, GOT LAND TERRAIN WARNING THROUGH 3000 FEET, 50 MILE (APPROX) MAP SHIFT OCCURRED. LOST VOR UPDATING - FMC MSG "PURGE UPDATE POS 2" CAME ON, COULD NOT RESET LNAV, RETURNED TO KIX. SWAPPED NR 1 ATC ANTENNA AND NR 1 DME ANTENNA REPLACED NR 1 FMC IAW B767 MM 34-61-01.