N650GT

Part: PRESSURE SWITCH — DEFECTIVE (LT ENGINE) · airframe 94,831 hrs · 28,440 cycles

ON TAXI OUT, LT ENGINE OIL FILTER STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE DIFFERENTIAL PRESS OIL SWITCH IAW AMM 79-35-01. OPS AND LEAK CHECKED GOOD. ACCOMPLISHED IDLE RUN OF NR 1 ENGINE IAW AMM 71-00-00. NO FAULTS PRESENT, ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAULTED (AUTOTHROTTLE SYS) · airframe 94,757 hrs · 28,396 cycles

DURING CRUSE,RIGHT AUTOTHROTTLE STAYS AT IDLE WHILE LEFT ADVANCES ENOUGH TO THROW PLANE OFF COURSE. AFTER SAFE LANDING MTX DEFERRED THE AUTOTHOTTLE SYSTEM IAW MEL 22-30-1. MX PROCEDURES COMPLIED WITH PLACARDS INSTALLED MBCB 11/24/25 REF. LOG PAGE 39215-93/1 A/C RETURNED TO SERVICE

Part: SENSOR — MALFUNCTIONED (LT ENGINE) · airframe 94,718 hrs · 28,380 cycles

FL320 L ENG STARTED SURGING, EPR +/- .55, N1 +/- 2.3, EGT +/- 20. FOLLOWED QRH, ENGINE STABILIZED IN "FLT" IGN. MODE- REMAIN MOSTLY STABLE. ANY TURB, R ENG SURGED ALSO. INTERMITTENT SURGE FOR REMAINING FLIGHT. DIVERTED TO CVG AND LANDED .MTX GROUNDED AC AND BEGAN TROUBLE SHOOTING. REMOVED AND REPLACED TT2 SENSOR I.A.W. B767 AMM 73-21-05. OPS CHECKED LH ENG TT2 SENSOR IAW B767 AMM 73-21-05. OPS CHECK GOOD. NO LEAKS NOTED. OPERATED #1 ENG AT VARIOUS POWER LEVELS IAW B767 AMM 71-00-00. OPS CHECK GOOD. A/C REMAINS NO ETOPS. MTX RETURNED AC TO SERVICE

Part: ESCAPE REEL — DETACHED (ZONE 200) · airframe 94,681 hrs · 28,356 cycles

DURING CREW PRE-FLIGHT CHECK, INERTIAL REEL FELL OUT OF HOLDER AS I WAS CHECKING IT. REMOVED AND REPLACED #4 INERTIAL REEL IAW B767 AMM 25-61-03. AIRCRAFT RETURNED TO SERVICE.

Part: ANTI-SKID VALVE — DEFECTIVE (ZONE 700) · airframe 94,636 hrs · 28,333 cycles

ON TAXI OUT, RH HYD QUANTITY WENT TO RF ON STATUS PAGE AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE REMOVED AND REPLACED RH ANTI-SKID MODULE IAW B76Y7 AMM 32-42-02. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELT — EXPIRED (ZONE 200) · airframe 94,629 hrs · 28,330 cycles

MAINTENANCE FOUND PORTABLE ELT BATTERY EXPIRED AUG. 2025. FWD TO MEL 23-24-1-1 NO DE-ACT PROCEDURES REQ MCCB 20JAN26 DI 66384 PLACARD INSTALLED. PORTABLE ELT REMOVED AND REPLACED IAW CMM 25-63-01 OPS CHECK GOOD. DI CLEARED. REMOVED PLACARDS NO MAINTENANCE ACTION REQUIRED. REF: L/P 39232-93/1. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTED · airframe 94,616 hrs · 28,326 cycles

ON TAXI OUT, WARN ELEX MSG APPEARED AND WAS UNABLE TO RESET. ACFT RETURNED TO THE GATE (BTB) AND MAINTENANCE GROUNDED ACFT , MTX PERFORMED BITE PROCEDURES 31-51 TREE 801 MSG CLEARED A/C OK FOR SERVICE. ACFT RETURUNED A SECOND TIME AND MESSAGE WAS CLEARED, FOUND A MODULE M616 AT FAULT, RESET OPS CHECK NORMAL IAW AMM 34-27-00. AND RETURNED ACFT TO SERVICE.

Part: SENSOR — DEFECTIVE (LT ENGINE) · airframe 94,567 hrs · 28,296 cycles

L ENG FLUCTUATE AT FL 360 EPR 1.31-1.27, N1 82.8-86.5, EGT 418-416. NO FLUCTUATION ON DESCENT OR APPROACH. DEFERRED THE EEC (PMC) SYSTEM PER MEL 73-21-1-1B. REACTIVATED EEC'S PER MEL 73-21-1-1B. REMOVED OLD, THEN INSTALLED NEW L ENGINE TT2 FUEL CONTROL SENSOR PER AMM 73-21-05. CONDUCTED ENGINE TEST PER AMM 71-00-00/501. LEAK CHECK OK. DI 65928 CLEARED REACTIVATION C/W. AIRCRAFT RETURNED TO SERVICE.

Part: ESCAPE REEL — DETACHED (ZONE 200) · airframe 94,562 hrs · 28,295 cycles

EMERGENCY DESCENT DEVICE IN COCKPIT #3 POSITION PREVIOUSLY DEPLOYED. REMOVED AND REPLACED #3 COCKPIT EMERGENCY DECENT DEVCE IAW AMM 25-61-03. REPLACED 4 EACH WORN RETENTION SPRINGS IAW B767 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SERVO — INOPERATIVE (ZONE 300) · airframe 94,551 hrs · 28,286 cycles

AFTER TAKEOFF, AIRCRAFT FISHTAILED (YAW LEFT TO RIGHT) RETURNED BACK TO KCVG,(ATB) AND DECLARED EMERGENCY.PERFORMED A SMOOTH OVERWEIGHT LANDING AT 305,000 LBS. ADDITIONAL "R YAW DAMPER" CAUTION AT FINAL APPROACH . MTX GROUNDED A/C ,TROUBLE SHOT AND REPLACED RIGHT YAW DAMPER SERVO, M509, PER B767 AMM 22-21-02.  SYSTEM CHECKS NORMAL.  OVERWEIGHT INSPECTION TRANSFERRED TO ITEM 38994-33/2. PERFORMED PHASE 1A OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35. NO DEFECTS NOTED MTX RETURNED A/C TO SERVICE.

Part: ESCAPE REEL — DETACHED (ZONE 200) · airframe 94,513 hrs · 28,267 cycles

MAINTENANCE FOUND #7 EMERGENCY DESCENT DEVICE FELL OUT OF IT'S CASE AND UNWINDED THE CABLE. (SUPERNUMERARY). REMOVED AND INSTALLED #7 EMERGENCY DESCENT DEVICE IAW AMM 25-61-03. AIRCRAFT RETURNED TO SERVICE.

Part: INERTIA REEL — LOOSE (ZONE 200) · airframe 94,439 hrs · 28,219 cycles

DURING POST FLIGHT INSPECTION, FOUND INERTIA REELS #4 AND #7 (SUPERNUMERARY) DROPPED TO FLOOR. DEFERRED #4 AND #7 INERTIA REELS IAW MEL 25-61-1-1. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 08/02/2025. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (ANTI-SKID SYS) · airframe 94,425 hrs · 28,210 cycles

DURING TAXI OUT, ANTI-SKID EICAS MSG AND OVRHD ANTI SKID-LIGHT INOP ON. AIRCRAFT RETURNED TO BLOCKS. (BTB). DEFERRED ANTI-SKID SYS IAW MEL 32-42-1. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 07/25/2025. AIRCRAFT DOWNGRADED TO CAT IIIA. A/C RETURNED TO SERVICE.

Part: SWITCH — OUT OF POSITION (VMO) · airframe 94,365 hrs · 28,164 cycles

DURING CLIMB, SPEED LIMIT INDICATION WAS 268 KT ALL TIME. AIRCRAFT AIR TURN BACK TO CVG. (ATB) MAINTENANCE FOUND VMO SWITCH IN ALT, PLACED IN NORMAL IAW AMM 32-00-00, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ESCAPE REEL — UNLATCHED (ZONE 200) · airframe 94,358 hrs · 28,157 cycles

EMERGENCY ESCAPE DEVICE REELS DISCOVER UNLATCHED AFTER LANDING AC GROUNDED. MTX DEFERRED #4,6,7 DEVICES IAW MEL ABX 25-61-1-1. AND DISPACHED A/C . LATER REPLACED #4,6,7 DESCENT DEVICES IAW B767 AMM 25-61-13 AND CLEARED DEFERRAL ON LOG PAGE 390056/1. RETURNED A/C TO SERVICE

Part: ENGINE — HOT START (RIGHT) · airframe 94,362 hrs · 28,161 cycles

RH HOT ENGINE START DURING TAXI OUT ,A/C RETURNED TO GATE(BTB) AND MTX GROUNDED A/C ,CREW MOTORED ENG TO LET COOL PER FIM 71-08 FAULT TREE 801. 2ND ENGINE START SUCCESSFUL. EGT PEAK 476.MTX RETURNED AC TO SERVICE .

Part: EGT INDICATION — READS HIGH (LT ENGINE) · airframe 94,292 hrs · 28,119 cycles

ON TAXI OUT, ATTEMPTED NORMAL START ON LEFT ENG, EGT WAS HIGH. ABORTED START. ACCOMPLISHED QRH PROCEDURE. SECOND ATTEMPT WAS HIGH EGT AND ABORTED. NO EXCEEDANCE OF EGT. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE PERFORMED IGNITION SYSTEM AUDIBLE TEST IAW AMM 74-00-00. OPS CHECK GOOD. A/C RETURNED TO SERVICE.

Part: PUMP — WARNING MESSAGE (ZONE 400) · airframe 94,282 hrs · 28,112 cycles

ON TAXI OUT AND ENGINE START, L FWD PUMP WHILE ENGINE ON IDLE WAS ON WITH EICAS MESSAGE. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED SYSTEM IAW MEL ABX-28-22-1. AIRCRAFT RELEASED TO SERVICE.

Part: ENGINE — OVERTEMP (LEFT) · airframe 94,239 hrs · 28,084 cycles

ON TAXI OUT, DURING LEFT ENGINE START EGT REACHED 541 EGT. AIRCRAFT RETURNED TO BLOCKS (BTB). PER AMM 71-00-00 AND FIM 71-08 FT 816. MOTORED LT ENGINE AND LET COOL. RESTARTED LT ENGINE, MAX EGT DURING START WAS 399 DEGREES. AIRCRAFT RELEASED FOR SERVICE.

Part: VALVE — MALFUNCTIONED (ZONE 300) · airframe 94,139 hrs · 28,024 cycles

AFTER PUSHBACK DURING TAXI & ENGINE START WE HAD A RUDDER RATIO EICAS MSG WITH DISCREAT LIGHT/A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX TROUBLESHOT AND T/S AS PER FIM 27-09 FT 814 PCA FAULT IN VIEW ON BOTH RRCM AFTER L AND R ENG START. REMOVED AND REPLACED LT HYD SYSTEM CENTER RUDDER PCA ASSY PER REF B767 AMM 27-21-02. PERFORMED LT PCA ADJUSTMENT AND RUDDER PCA TEST PER REF AMM 27-21-00, 27-21-02, LEAK TEST, NO LEAK NOTED RII 27-24-1 C/W. LP 39074-60 ITEM 2

Part: PROXIMITY SWITCH — MALFUNCTIONED (ZONE 200) · airframe 94,006 hrs · 27,940 cycles

DURING CLIMB AFTER T/O ENTRY DOOR, EMER DOORS, CARGO DOOR LIGHT OVERHEAD ANNUNCIATOR LIGHTS CAME ON, AND AC RETURNED TO FIELD (ATB) . AC RETURNED TO GATE AND MTX GROUNDED AC , TROUBLE SHOT AND REMOVED AND REPLACED PROXMITY SWITCH ELECTROME UNIT PER AMM 32-09-04. OPS CK GOOD NO DEFECTS NOTED.DURING CLIMB AFTER T/O ENTRY DOOR, EMER DOORS, CARGO DOOR LIGHT OVERHEAD ANNUNCIATOR LIGHTS CAME ON, AND AC RETURNED TO FIELD (ATB) . AC RETURNED TO GATE AND MTX GROUNDED AC , TROUBLE SHOT AND REMOVED AND REPLACED PROXMITY SWITCH ELECTROME UNIT PER AMM 32-09-04. OPS CK GOOD NO DEFECTS NOTED.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 93,959 hrs · 27,910 cycles

AT ENGINE START UP, RIGHT ENGINE OVERTEMP ON START UO - TEMP REACHED 545 DEG C. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE GROUNDED THE AIRCRAFT. MAINTENANCE TROUBLE SHOT IAW B767 FIM 71-05 FAULT TREE 801 AND FIM 71-08 FAULT TREE 816. ENG EXC PG ON EICAS SHOWED ENG 2 MAX EGT OF 545 DEG C FOR 0.1 SECONDS. PERFORMED EEC BIT CHECK IAW B767 FIM 71-01 FAULT TREE 8404. NO FAULTS NOTED AT THAT TIME. PERFORMED AUTO EVENT MSG CHECK AND CLEARED IAW B767 FIM 71-08 FT 810. NO FURTHER DISCREPANCIES. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 93,939 hrs · 27,894 cycles

L1 DOOR INDICATE OPEN DECLARED AND EMERGENCY AND DIVERTED AC TO KIND AND LANDED SAFELY .MTX GROUNDED AC AND .PERFORMED L1 DOOR RIGGING CHECKS IAW AMM 52-11-00. NO DESCREPANCYS FOUND. PERFORMED L1 DOOR SEAL INSPECTION IAW AMM 52-04-01, NO DEFECTS NOTED. PERFORMED PRECAUTIONARY LEAK CHECK TO 4 PSI IAW AMM 51-11-00. NO FAULTS NOTED. T/S CONT. ON L/P# 39008-96 ITEM 1 AND RETURNED AC TO SERVICE

Part: PRESSURE BLKHD — UNKNOWN (ZONE 100) · airframe 93,923 hrs · 27,880 cycles

DURING CURRENT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE ONE REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD WEB P/N 148T2610-156 AND BETWEEN R18-R19 AND BELOW OF TS4. THE REPAIR DOUBLER HAS BEEN REMOVED TO ASSESS THE DAMAGE. SEE FIGURE 1 FOR MORE DETAILS. THE PREVIOUS REPAIR DOES NOT MEET THE CONDITIONS PER B767-200 SRM, THEREFORE; BOEING WAS CONTACTED FOR REPAIR APPROVAL VIA SR: PEF-ABX-24-0105-01C MESSAGE. THIS REPAIR IS APPROVED BY FAA 8100-9 FORM. REPAIRED IAW ABX-REA-5380-65334-00 .

Part: PRESSURE BLKHD — UNKNOWN (ZONE 100) · airframe 93,923 hrs · 27,880 cycles

DURING CURRENT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE ONE REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD WEB P/N 148T2610-156 AND BETWEEN R20-R21. THE REPAIR DOUBLER HAVE BEEN REMOVED TO ASSESS THE DAMAGE. SEE FIGURE 1 FOR MORE DETAILS. THE PREVIOUS REPAIR DOES NOT MEET THE CONDITIONS PER B767-200 SRM, THEREFORE; BOEING WAS CONTACTED FOR REPAIR APPROVAL VIA SR: PEF-ABX-24-0104-01C MESSAGE. THIS REPAIR IS APPROVED BY FAA 8100-9 FORM REPAIRED APB BETWEEN RS20-21 TO FABRICATED, LOCATED, DRILLED NEW PARTS AND INSTALLED FILLERS AND DOUBLER. IAW ABX-REA -5380-65333-00

Part: SKIN — DENTED (ZONE 100) · airframe 93,923 hrs · 27,880 cycles

DURING CURRENT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED A DENT ON THE FUSELAGE SKIN BETWEEN STATIONS 1395-1417 AND BETWEEN S-28L AND S-29L. THE DENT WAS FOUND TO BE OUT OF SRM ALLOWABLE LIMITS. 767-200 SRM 53-00-01 REPAIR 1 REQUIRES THE DOUBLER REPAIR TO BE AT LEAST 22 INCHES FROM A SKIN CUTOUT. THIS REPAIR WILL BE INSTALLED ALL THE WAY TO THE BULK CARGO DOOR CUTOUT, THEREFORE; ENGINEERING WAS CONTACTED FOR REPAIR APPROVAL. THIS REPAIR IS APPROVED BY FLIGHT VEHICLES CONSULTING, INC. (FVCI). PERMANENT REPAIR INSTALLED IAW ABX-REA-5365-65332-00.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 93,923 hrs · 27,880 cycles

DURING C-CHECK AT TAMPA MTX FOUND CORROSION COMMON TO STRINGER 33L AT STA.1576 ON BULK CARGO, COMPARTMENT INTERNAL SURFACE. THE STRINGER (P/N 146T3002-47) IS MADE FROM THE -267 WHICH IS M/F 0.140" THK 7075-0 BARE SHEET PER QQ-A-250/12, HT TO -T6. THE STRINGER THICKNESS AT THE DAMAGEL OCATION IS 0.100” PER BAC DWG 146T3002 SHT 3. THE DAMAGE IS REPAIRABLE PER B767-200 SRM 53-00-03,REPAIRED IAW SRM 53-00-03 REPAIR 2 DETAIL IV ., ABX REA-5300-65575-00.AND ABX-REA-5300-65575-01

Part: TRANSMITTER — MALFUNCTIONED (ZONE 200) · airframe 90,712 hrs · 27,831 cycles

DURING FLIGHT FROM CVG TO ELP WX RADAR FAILED AND AIRCRAFT DECIDED TO RETURN TO CVG .AC LANDED AND MTX GROUNDED AC . MTX TROUBLESHOT AND REPLACED WEATHER RADAR TRANSCEIVER IAW B767 AMM 34-43-01 OPS CHECK GOOD . MTX RETURNED AC TO SERVICE

Part: CONTROL PANEL — MALFUNCTIONED (ZONE 200) · airframe 93,904 hrs · 27,864 cycles

ATC FAIL LIGHT ILLUMINATED DURING PUSH BACK AC RETURNED TO GATE AND MTX GROUNDED AC, MTX TROUBLE SHOT THEY REMOVED AND REPLACED TRANSPONDER CONTROL PANEL IAW B767 AMM 34-53-02 OPS CHECK GOOD MTX RETURNED AC TO SERVICE .

Part: SENSOR — MALFUNCTIONED (ZONE 500) · airframe 93,897 hrs · 27,859 cycles

IN CRUISE AT FL350, LT ENG SURGING .3 N1 INCREASING TO .6 N1 FLUXUATION BY THE TIME OF SHUTDOWN IAW QRH. FLUXUATION REFLECTED IN EPR, FF, & OIL PRESS. PER QRH. ENG SHUTDOWN & CREW DECLARED AN EMERGENCY & DIVERTED TO DFW . AFTER LANDING MTX GROUNDED ACFT. PERFORMED LT ENG RUN UP IAW AMM 71-00-00. PERF OPS CHECK OF LT ENG EEC ON & OFF IAW AMM 73-21-07. CONDITION REMAINS, INDICATION FLUCTUATED EITHER EEC ON OR OFF. C/W FIM 71-05 FT 822. INSPECTED ENG OIL CHIP DETECTOR, NO CONTAMINATION. INSPECTED MAIN OIL FILTER, NO CONTAMINATION. R & R TT2 SENSOR IAW AMM 73-21-05 PER FIM 73-21-FT 811. PERFORMED ENG RUNS IAW 71-00-00. ADJUSTED MIN IDLE IAW AMM 71-01-00 TO MATCH TRIM TABLE. OPS CHK GOOD. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLAPS) · airframe 90,524 hrs · 27,677 cycles

AFTER TAKE UPON RETRACTING FLAPS TO UP POSITION SO LEADING EDGE SLAT ASYMMETRY EICAS, CAUTION. ACCOMPLISHED NON-NORMAL RETURNED FOR LANDING IN CVG AFTER LANDING MTX GROUNDED A/C AND FOUND FSEU WITH "LVRI NOT IN DETENT" 27-51040. ACCOMPLISHED M604 RUDT ADJUSTMENT IAW B767 AMM 27-51-26. OPS AND BITE CHECK GOOD. CYCLED FLAPS AND SLATS, NO FAULTS AT ANY POSITION AND RETURNED AC TO SERVICE AND DEPARTED .

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENG STARTER) · airframe 90,483 hrs · 27,642 cycles

DURING TAXI OUT #2 ENGINE STARTER EICAS MESSAGE DISPLAYED DURING ENGINE START.AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC CREW PERFORMED A SECOND ATTEMPT TO STAR RH ENGINE ENG STARTED SUCCESSFUL PER ENGINE RUN PROCEDURES AMM 71-00-00.MAINTENANCE RETURENED TO SERVICE ,

Part: FUEL CONTROL — FAULTED (LT ENGINE) · airframe 93,818 hrs · 27,794 cycles

L ENG EPR, N1 EGT FLUCTUATED IN FLIGHT. SEE VIDEO SENT MECH/MTC AC RETURED TO FIELD AND GROUNDED BY MAINTENANCE DETERMINED FROM FLIGHT DATA AND NAMED VIDEO THE L ENGINE FUEL CONTROL FAULTY, REMOVED NAMED PART PER AMM 73-21-01. DETERMINED FROM FLIGHT DATA AND NAMED VIDEO THE L ENGINE FUEL CONTROL FAULTY, REMOVED AND REPLACED NAMED PART PER AMM 73-21-01.OPS CHECK GOOD

Part: BEAR STRAP — CORRODED (BS 1260 S23-24R) · airframe 93,783 hrs · 27,771 cycles

AIRBORNE MAINTENANCE AT CVG DISCOVERED CORROSION ON THE INTERNAL BEARSTRAP (P/N 146T8521-1) LOCATED AT THE AFT LOWER CARGO CONTROL PANEL SKIN CUTOUT AT APPROXIMATE STATION 1260 BETWEEN S-23R TO S-24R.THE CORROSION WAS REMOVED PER 767-200 SRM 53-30-15, REPAIR 1, AND EXCEEDS 10% MATERIAL LOSS. A UT INSPECTION WAS ACCOMPLISHED TO DETERMINE THE MATERIAL THICKNESS AND RECORDED IN A 0.25" X 0.25" GRID PATTERN.INSPECTION REPORTED A 0.143" MINIMUM REMAINING MATERIAL THICKNESS AT THE THINNEST LOCATION (EOP) FROM 0.212"NOMINAL (0.069” OR 32.55% REMOVED). AMES ENGINEERING CONTACTED FLIGHT VEHICLES CONSULTING INC. FOR FURTHEREVALUATION AND APPROVAL.DEFER PER THIS REA FOR MAINTENANCE TRACKING PER GMM CHAPTER 1,SECTION 07.04. PERMANENTLY REPAIR THE BEAR STRAP ON OR BEFORE 25 FLIGHT CYCLES. C/W REA ABX-REA-5300-65395-01 AND NR WORK PACK W/O 12105189. DEFERRED IAW REA -5300*65395-01 AND ABX GMM 07.04 FOR TRACKING MBCB 25 CYCLES

Part: ADC — MALFUNCTIONED (LEFT) · airframe 93,696 hrs · 27,716 cycles

LEFT AIR DATA COMPUTER FAULED IN FLIGHT AT FL390. UNRELIABLE AIRSPEED, UNRELIABLE ATLTITUDE, AILERON LOCKOUT AND RUDDER RATIO CALL INDICATION ON EICAS PILOT DECLARED AN EMERGANCY AND LANDED . MAINTENANCE GROUNDED AC. TROUBLE SHOT AND REPLACED LH ADC IAW 34-12-01 OPS CHECK GOOD AC REMAINS NON RVSM PENDING HIGH RANGE LEAK CHECK . AND RETURNED AC TO SERVICE.

Part: PITOT HEAD — MALFUNCTIONED (FIRST OFFICER'S) · airframe 93,672 hrs · 27,704 cycles

WHILE STARTING ENGINE DURING TAXI "FIRST OFFICER PITOT" APPEAR ON EICAS. AC RETURED TO GATE AND AC WAS GROUNDED BY MAINTENANCE ,PERF FIM 30-31 FT 803, REMOVED AND REPLACED K646 R PROBE HT NZ RELAY PER BSWPM 20-81-22, AND WDM 30-31-21. PROBE HT OPS CK GOOD OUT PANEL P61 PER AMM 30-31-00. PERF RH ENG GROUND IDLE PER AMM 71-00-00 EICAS MSG RETURNED AND LT. RE-PERFORMED FO'S PITOT PROBE TEST WHILE RECORDING TEMP, PROBE HT TEST FAILS PER AMM 30-31-00. REMOVED AND REPLACED FO'S PITOT PROBE PER AMM 34-11-01. PERF HIGH RANGE LEAK CK. LEAK CHECK GOOD. PERF RH ENG GROUND IDLE TEST PER AMM 71-00-00, OPS CK GOOD. AC RETURNED TO SERVICE

Part: VANE — MALFUNCTIONED (ENGINE VANE) · airframe 93,646 hrs · 27,689 cycles

WHILE SETTING THRUST DURING A STATIC TAKEOFF WITH EEC'S DEFERRED A COMPRESSOR STALL OCCURRED. THE COMPRESSOR STALL SEEMED TO BE ON THE LT ENG, ABORTED TAKE OFF AND RETURNED TO THE GATE.MAINTENANCE GROUNDED AC ,MAINTENANCE T/S IAW FIM 71-05 F/T 806. PERFORMED BORESCOPE OF #1 ENG IAW AMM 72-00-00 NO DEFECTS NOTED.#2 ENGINE STILL IN WORK .AMENDED REPORT WILL BE FILED AFTER COMPLETION .#2 ENGINE BORO. FOUND 11TH STAGEL/PC WITH LEADING EDGE DAMAGE. REPAIRED IAW AIM W/O 24-01-22-01R .RIGHT ENGINE VSV ACTUATOR LEAKING FROM DRAIN. REPLACED IAW 75-31-02. LEFT ENGINE EVBC INPUT LEVER LEAKING FUEL.REPLACED EVBC IAW 75-31-01 PERFORMED ENGINE TRIM RUNS OPS CHECK GOOD IAW 71-01-00/501 PERFORMED EVAL FLIGHT SATISFACTORY.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 93,608 hrs · 27,667 cycles

RUDDER AND RUDDER TRIM CONTROL SYSTEM: RUDDER TRIM. FAILED TO TRIM IN EITHER DIRECTION A/C RETURNED TO GATE.MAINTENACE GROUNDED A/C. BEGAN TROUBLESHOOTING ,TRIED NEW CONTROL PANEL, NO HELP. RE-INSTALLED ORIGINAL. RANG, MEGGER AND LOAD CHECKED RUDDER TRIM WIRING IAW WDM 27-21-11, NO DEFECTS NOTED. REMOVED AND RPELACED RUDDER TRIM ACTUATOR IAW B767 AMM 27-21-11. OPS CHECK GOOD. C/W RII 27-08 RETURNED AC TO SERVICE .

Part: UNKNOWN — HANDLER ERROR (UNKNOWN) · airframe 93,567 hrs · 27,643 cycles

DURING PUSH BACK A/C TOW BAR BROKE MAINTENACE GROUNDED AC AND RETURNED TO BLOCKS WITH SERVICABLE TOW EQUIPTMENT TO PERFORM INSPECTION PHASE 1 MAX NLG TOW ANGLE EXCEEDANCE INSPECTION IAW AMM 05-51-29.NO FINDINGS NOTED A/C RETURNED TO SERVICE AND DISPATCHED.

Part: CONTROL CARD — MALFUNCTIONED (BLEED SYSTEM) · airframe 93,486 hrs · 27,590 cycles

LH BLEED OFF LIGHT DID NOT EXTINGUISH A/C RETURNED TO BLOCKAND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED LH ENG PRSOV PER AMM 36-11-09 AND SWAPPED AIR BLEED CONTROL CARDS (LH&RH), NO HELP, SWAPPED CARDS BACK TO ITS ORIGINAL POSITION REFERENCE AMM 36-11-12. DURING ENG (LH) RUN OBSERVED PRSOV OPEN/CLOSES AS COMMANDED WITH THE LH "BLEED" SW ON P5, BUT NO DUCT PRESSURE AVAILABLE. PERFORMED AIR SUPPLY BITE TEST REF FIM 36-20 FT 809, DISPLAYED FAN AIR SENSOR FAULT LT & WIRE FAULT. REPLACED FAN AIR TEMP SENSOR REF AMM 37-11-07 STILL NO BLEED. CARRIED FORWORD TO NEXT ITEM. FOUND ON P5 OVHD PNL "S4" LH ENG BLEED PB WIRE "6" ON "9" LOCATION. PER WDM 36-11-61. "9" SHOULD BE BLANK, WIRE "6" SHOULD BE ON "6" LOCATION. VERIFIED WITH NEW PANEL. REMOVED AND REPLACED BLEED AIR OVHD PANEL ASSY. OPS CHECK GOOD. DUCT PRESS NOTED. "OFF" LIGHT EXTINGUISHED.A/C RETURNED TO SERVICE.

Part: EXCITER — DEGRADED (ZONE 600) · airframe 93,421 hrs · 27,548 cycles

#2 ENGINE WOULD NOT START ON APU.,ACCOMPLISHED APU OPS AND LEAK CHECK IAW B767 AMM 49-11-00. APU PNEUMATICS WORK GOOD IN ALL MODES. 30-35 PSI. IN MES. FOUND RH ISOLATION SLIP JOINT WITH PNEUMATIC LEAK, SEE LP 38740-91/1 FOR DUCT REPAIR FURTHER T/S REQUIRED. DURING #2 ENGINE INSPECTION FOUND BAD #1 IGNITER PLUG. REMOVED AND REPLACED RH ENGINE #1 IGNITER PLUG IAW B767 AMM 74-21-01. OPS CHECK GOOD. SEE LOG PAGE 38740-91 ITEM 1. PERFORMED OPS CHECK IAW B767 AMM 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED APU OPS CHECK GOOD IAW B767 AMM 49-41-00. DI CLEARED. PLACARD REMOVED. NO MX ACTION REQUIRED AT THIS TIME. REF LP 38740-92/2

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,355 hrs · 27,512 cycles

ON START RT ENGINE EGT EXCEEDED 500 DGREE + WAS CONTINUING TO CLIMB. NI 7.1%, NL APPROX 31 ABORTED ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED GUI OF R/ENG. NO DEFECTS FOUND. ENGINE RUN OPS CHECKED R/ENG PER FIM 71-08. F/T 816. NO DEFECTS NOTED. PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (LEFT ENGINE) · airframe 93,330 hrs · 27,500 cycles

ON DESCENT TO CVG (APPROXIMATELY 15,000 FT), THE L OIL FILTER EICAS MESSAGE APPEARED. QRH PROCEDURES WERE FOLLOWED WHICH LED TO SHUTTING DOWN THE LEFT ENGINE, DECLARING AN EMERGENCY AND LANDING AT CVG. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND OIL PRESSURE DIFFERENTIAL SWITCH DEFECTIVE. SWITCH WAS REPLACED IAW B767 AMM 79-35-01. OPS CHECK GOOD. NO MESSAGE PRESENT. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,271 hrs · 27,466 cycles

CREW REPORTED 2 FAILED START ATTEMPTS ON RIGHT ENGINE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED RT ENGINE START IAW B767 AMM 71-00-00, ENGINE STARTED NO ISSUES, MAX MOTOR OF 22% N2 AT LIGHT OFF. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,148 hrs · 27,391 cycles

AFTER L ENGINE START LEFT GEN DRIVE DISC SWITCH LIGHT REMAINED ILLUMINATED. L GEN OFF AND L GEN DISC EICAS MESSAGE. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED L/H GENERATOR PER MEL 24-00-1-3. MX PROCEDURES COMPLIED WITH. PLACARD INSTALLED. MBCB 22 APRIL 23. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,150 hrs · 27,392 cycles

R ENG FAILED TO START: HUNG START AT N2 31% ABORTED ENGINE START TWICE JUST BELOW EGT LIMIT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED #2 ENG AND RESTARTED AT GATE PER AMM 71-00-00 IGNITION NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 93,033 hrs · 27,327 cycles

NOSE GEAR AIR/GROUND STATUS MSG DISPLAYED DURING CLIMB. AIR TURN BACK INTO TPA WITHOUT FURTHER INCIDENT. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE ADJUSTED SENSORS S266 AND S244 ON NLG OP TEST GOOD IAW B767 AMM 32-09-08-822-044 32-09-08-702-014. AIRCRAFT RETURNED TO SERVICE

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 93,033 hrs · 27,326 cycles

DURING TAXI, PLANE PULLS TO THE LEFT, REQUIRED TWO UNITS OF TILLER OR HALF RUDDER TRAVEL TO MAINTAIN CENTERLINE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE ADJUSTED CABLES, CHECKED TENSION. ALL RIG PINS ALIGN FREELY IAW B767AMM 32-57-00. AIRCRAFT RETURNED TO SERVICE.

Part: ANTENNA — MISLOCATED (ZONE 200) · airframe 93,033 hrs · 27,326 cycles

DURING C CHECK, MAINTENANCE WAS REQUIRED TO INSTALL AN ELT ANTENNA (STC# ST02929AT) PER EMTEQ DRAWING 2-32669-701. MAINTENANCE HAS INSTALLED THE ELT ANTENNA DOUBLER IN THE STA 1503 IN LIEU 1506. ENGINEERING WAS CONTACTED FOR FURTHER EVALUATION. INSTALLATION ACCOMPLISHED PER ABX-REA-2560-64899-01. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: ANTENNA — MISLOCATED (ELT) · airframe 930,033 hrs · 27,326 cycles

DURING C CHECK, MAINTENANCE WAS REQUIRED TO INSTALL AN ELT ANTENNA (STC# ST02929AT) PER EMTEQ DRAWING 2-32669-701. MAINTENANCE DISCOVERED THAT THE CONFIGURATION OF THE AIRCRAFT DID NOT MATCH THE INSTALLATION DRAWING SEE FIGURE 1. MAINTENANCE CONTACTED ENGINEERING FOR FURTHER EVALUATION. INSTALLATION WAS ACCOMPLISHED PER ABX-REA-2560-64899-00 VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,033 hrs · 27,326 cycles

DURING AIRCRAFT C-CHECK AT AMS-TPA, MAINTENANCE WAS REQUIRED TO INSTALL AN ELT TRANSMITTER (STC# ST02929AT) PER EMTEQ DRAWING 2-32669-702. MAINTENANCE DISCOVERED THAT THE CONFIGURATION OF THE AIRCRAFT DID NOT MATCH THE INSTALLATION DRAWING. STRUCTURAL MEMBERS (REFERENCE. P/N 284T0199) EXTENDING VERTICALLY FROM FRAMES AT STATION 1540 AND STATION 1562 WERE NOT INSTALLED ON THE AIRCRAFT. MAINTENANCE CONTACTED ENGINEERING FOR FURTHER EVALUATION. INSTALLATION ACCOMPLISHED PER ABX-REA-2560-64900-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR

Part: STIFFENER — DAMAGED (RIGHT ENGINE) · airframe 93,033 hrs · 27,326 cycles

DURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED DAMAGE TO THE AFT STIFFENER ON THE #2 ENGINE INBOARD THRUST REVERSER. DAMAGE WAS CAUSED BY IDG FEEDER CABLE(S) SHORTING AND ARCING TO THE STIFFENER. AN INTERIM REPAIR WAS ACCOMPLISHED BY LINE MX PER ABX-REA-7830-64869-00, AND THE INTERIM REPAIR IS SCHEDULED TO BE REPLACED BY A PERMANENT REPAIR AT THIS MX VISIT. THE AFFECTED STIFFENER (315T3100-8) IS MADE FROM BAC1506-3279 PROFILE (2219-T62 MATERIAL). THE DAMAGED VERTICAL FLANGE OF THE STIFFENER IS 0.090” THICK. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. REPAIRED PER ABX-REA-7830-64792-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: NONE — NONE · airframe 92,917 hrs · 27,258 cycles

NO LIGHT OFF LEFT ENGINE WITH TWO ATTEMPTS. AIRCRAFT BACK TO BLOCK AND GROUNDED BT MAINTENANCE. MAINTENANCE STARTED L/H ENGINE IAW B767 AMM 71-00-00. LIGHT OFF ON FIRST ATTEMPT W/ BOTH IGNITORS SELECTED. AIRCRAFT RETURNED TO SERVICE.

Part: LEAD — FAULTED (NR 1 IGNITER) · airframe 92,881 hrs · 27,238 cycles

2 FAILED START ATTEMPTS ON LEFT ENGINE W/IGNITION IN BOTH. 3RD ATTEMPT STARTED L ENGINE USING #1 IGNITION. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE. RESET IGNITER LEAD #1, RUN #1 ENG OPS CK OK. A/C RETURNED TO SERVICE.

Part: IGNITION SYS — FAULTED (NR 1 ENGINE) · airframe 92,879 hrs · 27,235 cycles

3 FAILED START ATTEMPTS #1 ENGINE #2 IGNITION INOP. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED ENGINE RUN OF L/H ENGINE. MAINTENANCE DEFERRED # 2 IGNITION PER MEL74-00-1B. PLACARDS INSTALLED. NO MAINTENANCE PROCEDURES REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (RT ENG EGT) · airframe 92,820 hrs · 27,192 cycles

EGT EXCEEDANCE 538 ON RIGHT ENGINE DURING START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED ENGINE AND TURBINE AREA. NO DEFECTS NOTED IAW B767 AMM 72-51-01. AIRCRAFT RETURNED TO SERVICE.

Part: EXCITER — DEFECTIVE (LT ENGINE) · airframe 92,772 hrs · 27,155 cycles

LEFT NO LIGHT OFF WITH #2 IGNITION ACCOMPLISHED ABORTED ENG PROC. ATTEMPTED SECOND START IN BOTH, NO LIGHT OFF. FF=700 N2=24. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED #2 IGN EXCITER BOX IAW B767 AMM 74-11-01. PREFORMED ENGINE IDLE RUN. AIRCRAFT RETURNED TO SERVICE.

Part: EXCITER — FAILED (LEFT ENGINE) · airframe 92,523 hrs · 27,018 cycles

LEFT ENGINE WOULD NOT START WITH IGNITORS IN 2 OR BOTH. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED #1 EXCITER BOX AND LEAD, REF B767 AMM 74-11-01 + 74-21-01. OPS CHECK OF IGNITION SYSYEM CHECKS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 92,458 hrs · 26,985 cycles

R/H ENGINE EGT EXCEEDANCE ON START 542 DEGREES FOR 3 SECONDS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE T/S IAW FIM 71-08-00-990-816-P00. PERFORMED #2 ENG START WITH FLT CREW IAW AMM 71-00-00. SECOND ENG START WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.

Part: ANTI-ICE VALVE — BINDING (RIGHT ENGINE) · airframe 92,166 hrs · 26,859 cycles

RT ENGINE TAI VALVE AFTER START UP, STATUS MSG. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH ENG R TAI VALVE. IAW B767 30-21-03 OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 92,153 hrs · 26,854 cycles

RIGHT ENGINE FAILED TO START AFTER 2 ATTEMPTS. EGT 585 FOR 2.6 SECONDS. 593 MAX. AIRCRFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED ENGINE EGT ECEEDANCE FAULT ISOLATION IAW FIM 71-08 FAULT TREE 816 CHART AREA F. PERFORMED NORM ENGINE START IAW 767 AMM 71-00-00. IDLE EGT WITHIN NORMAL LIMITS. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 92,145 hrs · 26,850 cycles

R ENG TAI VLV STATUS MESSAGE ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLE SHOT IAW B767 FIM 30-21 FT705. OPERATED RH ENG. SYSTEM OPERATES NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: STARTER — SEIZED · airframe 92,102 hrs · 26,833 cycles

ON ENGINE START LEFT ENGINE STARTER EICAS ALONG WITH LEFT VALVEDISCRETE LIGHT. NO ROTATION. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED #1 ENGINE PNEUMATIC STARTER IAW B767 AMM 80-11-01. OPS CHECKED GOOD. AICRAFT RETURNED TO SERVICE.

Part: COMPUTER — INTERMITTENT · airframe 91,934 hrs · 26,766 cycles

EICAS MESSAGE RT EICAS INOP DISPLAYED, AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED R EICAS COMPUTER OPS CHECKED GOOD IAW B767 MM 31-41-02 AIRCRAFT RELEASED FOR SERVICE.

Part: NONE — NONE · airframe 91,851 hrs · 26,733 cycles

SPOILER EICAS MESSAGE ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND PINS "B14" OF "A" PLUG OF BOTH 2R + 3R SPOILER CONTROL MODULE IN WRONG PIN. MOVED TO "C" 14 OF BOTH PLUGS REPLACED SPOILER MODULE "1R" ALL SPOILER FUNCTIONS CHECK NORMAL REF B767 AMM 29-61-00. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (AILERON LOCKOUT) · airframe 91,851 hrs · 26,733 cycles

AFTER START AILERON LOCKOUT EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT IAW MEL 27-11-2 DI # 26214. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 91,845 hrs · 26,730 cycles

SPOILERS EICAS AND OVERHEAD DISCRETE LITE ON DURING CRUISE FLIGHT, AIRPLANE TURNED LEFT TWICE DURING THE LITE COMING ON. RIGHT HYD. QTY. DROPPED TO .64. AIR TURN BACK TO CVG WITH OUT FURTHER INCIDENT. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE DISCOVERED A CRACKED T FITTING AND WAS REPLACED IAW 20-10-09. AFTER CORRECTION OF R HYD QTY ISSUE, CONDUCTED OPERATIONAL TEST OF SPOILER TEST OF SPOILERS PER AMM 27-61-00/501. ALL SPOILERS OPERATE. OPS TEST OK PER FIM 27-09 FT 803, NO SPOILER MESSAGE PRESENT. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 91,842 hrs · 26,728 cycles

RT. ENG. IGNITION START SELECTOR DOES NOT HOLD IN THE GND POSITION WHEN STARTING. NO VALVE LIGHT, NO N2 ROTATION. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MINTENANCE. MAINTENANCE FOUND START CONTROL VALVE WAS FAULTY. START CONTROL VALVE WAS DEFERRED IAW ABX MEL 80-00-2-1. A MANUAL START WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

ON PROCESS INSPECTION OF REMOVAL, FOUND CORROSION ON INTERCOSTAL RBL 28 FROM STA 610 TO 635. REMOVED CORROSION FROM INTERCOSTAL STA 610-635 RBL 28 AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-04-1A-1. FABRICATED NEW INTERCOSTAL AND APPLIED PROTECTIVE FINISHES, IAW BOEING DWG 143T5000 REV AL,G , B767 SRM 51-20-01.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA HAS CHIPPED PAINT/POSSIBLE CORROSION ON SHEAR TIE, STA 720 AFT SIDE BETWEEN STRINGER 38L-37L. REMOVED CORROSION FROM SHEAR TIE AT FWD CRGO STA 720 38L-37L AND FOUND OUT OF LIMITS, IAW B767 SRM 51-10-02. REMOVED AND REPLACED SHEAR TIE, IAW B767 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPARTMENT BILGE AREA HAS CORRODED SHEAR TIE AT STA 698 BL 0. SHEAR TIE AT STA 698 BL 0 FOUND OUT OF LIMITS WITH 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR TIE, IAW B767 SRM 51-40-02, BOEING DWG 143T1212 REV D.

Part: SKIN — DELAMINATED (RT WING SLAT 11) · airframe 91,312 hrs · 26,458 cycles

RT WING SLAT NR 11 HAS DELAMINATION UNDER EXISTING REPAIR OUTBOARD END OF WEDGE. APPLIED REPAIR TO RT WING SLAT NR 11. REMOVED AREA OF DAMAGE 8.75X4.25, IAW B767 SRM 51-70-10-2R-0 PAR 7. FABRICATED DOUBLER & FILLER USING MATERIAL ID PN: 2024-T3 .016 PO NR FC 1900787 LOT L1162546, IAW B767 SRM 57-43-02-01 ID 1 FAB DOUBLER 5.75X10 FILLER 8.6X4.25, IAW B767 SRM 51-70-10-2R-0 PAR 8. APPLIED REPAIR, IAW B767 SRM 51-70-10 PAR 20 SEAL & PRIME, IAW B767 SRM 51-70-10 PAR 22. TOP COAT APPLY, IAW B767 AMM 51-21-10-307-020.

Part: SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO LOWER MAIN SILL RBL 44.9 AFT OF ST 605 TO STA 632 HAS CORROSION ON INNER CHORD AND UNDERLYING ATTACH STRUCTURE. INNER CHORD, FAIL SAFE STRAP AND 5 EA BACK UP FITTINGS FOUND OUT OF LIMITS. REMOVED AND REPLACED INNER CHORD, FAIL SAFE STRAP AND 4 EA BACKUP FITTINGS (STA 561.95), IAW B767 SRM 51-40-02-0G-0, FAS EA 20038 REV IR. REPAIRED 1 EA BACK UP FITTING (STA 545.5), IAW FAS EA 20039 REV IR AT STA 522-632 RBL 44.5 FWD CARGO LOWER SILL (BACKUP FITTINGS OFF PART: P/N 143T8022-3, NSN).

Part: FLOORBEAM — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO PIT FLOOR STA 742 BEAM LBL 23 IN BOTTOM AFT SIDE TOP FLANGE HAS 3 SQUARE IN OF EXFOLIATED CORROSION. REMOVED CORROSION ON BOTTOM SIDE OF FLANGE 'J' CHANNEL AT STA 742 LBL 23 IN AN AREA 6.5"X1", IAW B767 SRM 51-10-02. ORIGINAL MATERIAL 100, REMAINING .038, LOSS .062 OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-1 FIG 101 DETAIL VIII ASSET NR 0011938 CAL DUE 21APR21. REMOVED 'J' CHANNEL AND REPLACED P/N 1506-3121 7075-T6511 P/O FS20075 63, IAW B767 SRM 51-40-02.

Part: STRINGER — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT OF FWD CARGO PIT STA 774 STR 37R HAS 3 SQ IN EXFOLIATED CORROSION. STR 37R AT STA 774 FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 37R, IAW B767 SRM 53-00-03-2R-2.

Part: FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, TOP OF FRAME SUPPORT HAS CORROSION ON UPPER SUREFACE STA 540 S35R. REMOVED CORROSION FROM FAIL SAFE STRAP STA 540 STR 35R AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-1. REPAIRED FAIL SAFE STRAP, IAW FAS EA 20034 REV IR.

Part: THRESHOLD — CORRODED (BULK CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

BULK CARGO DOOR BOTTOM FWD CUTOUT ON FUS SUB THRESHOLD SUPT ABOVE EXT, FUSE SKIN CORRODED 3 SQUARE IN. STIFFNER LOCATED AT BULK CARGO DOOR BOTTOM FWD CUTOUT AT FUSE SUB THRESHOLD ABOVE EXT FUSE SKIN HAS 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-15-01-3. REMOVED AND REPLACED STIFFNER, IAW B767 SRM 53-60-15-01-3. RESTORED PROTECTIVE FINISHES, IAW B767 SRM 51-20-01.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE, SHEAR TIE CORRODED ON FWD SIDE, STA 500 S39L-38L. REMOVED CORROSION FROM SHEAR TIE STA 500 S39L-38L AND FOUND 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 51-10-02, 53-00-07-1A-1. REMOVED AND REPLACED SHEAR TIE, IAW B767 SRM 51-40-02, BOEING DWG 143T1203 REV D.

Part: SKIN — DELAMINATED (RT WING SLAT 12) · airframe 91,312 hrs · 26,458 cycles

RT WING NR 12 SLAT HAS LARGE DELAMINATED ON OUTBOARD SIDE OF WEDGE. REPAIRED NR 12 SLAT OUTBOARD SIDE OF TRAILING EDGE WEDGE, IAW B767 SRM 51-70-10-2R-4.

Part: STRINGER SPLICE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, LIGHT CORROSION INSIDE STRINGER SPLICE STA 434 STR 33L. REMOVED CORROSION FROM FWD CARGO BILGE AREA STA 434 STR 33L STRINGER SPLICE AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07. REMOVED AND REPLACED STRINGER SPLICE AT STA 434 33L, IAW B767 SRM 51-40-02, 53-00-03-2R-2. RESTORED PROTECTIVE FINISHES, IAW B767 SRM 51-20-01.

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD PIT CORROSION ON MAIN FRAME AFT DOOR JAMB AT THRESHOLD. EVALUATED 615.5 FRAME LOWER CHORD STR 33R-34R AND FOUND 100% OUT OF LIMITS AND REPAIRED, IAW FAS EA 20036 REV IR.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPARTMENT BILGE AREA STRINGER 37R HAS AREA OF CORROSION AT BS 453. FOUND CORRODED AREA AT FWD CARGO COMPARTMENT STRINGER 37R BS 453 WITH MATERIAL LOSS 100%, TO BE OUT OF LIMITS, IAW B767 SRM 53-00-03. CUTOUT DAMAGED SECTION DIM. 30.5". FABRICATED AND INSTALLED NEW STRINGER SECTION FROM BAC 1498-205 P/O FS1808920 DIM 30.5" AND SPLICE REPAIR FROM BAC1498-201 P/O FS 1916622 DIM 13.7, IAW B767 SRM 53-00-03 REP 2.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FLOOR SUPPORT STRUCTURE HAS CORROSION FROM STA 610-STA 632 AND RBL 38-RBL 24. FLOOR SUPPORT STA 610-632 RBL 24-38 FOUND 100% MATERIAL LOSS AND FOUND OUT OF LIMITS. NEW FLOOR SUPPORT PN 143T5000-34 WILL BE INSTALLED ON NR-00891, PER CUSTOMER REQUEST. CORROSION ON J-CHORDS AT STA 610 AND 632 RBL 24-38 FOUND OUT OF LIMITS AND REPAIRED, IAW B767 SRM 53-00-07-2R-4.

Part: FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD PIT-CORROSION ON UNDERSIDE OF FRAME FLANGE AT STA 522 LBL 42. UPON EVALUATION OF FRAME J CHORD STA 522 LBL42, FOUND 100% OUT OF LIMITS AND REPAIRED, IAW B767 SRM 53-00-07-2R-4.

Part: FRAME — CORRODED (APU DOOR) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

RT APU ACCESS DOOR 5TH FRAME FROM FWD END OF DOOR HAS CORROSION ON AFT SIDE OF FRAME INBOARD CORNER. REMOVED CORROSION ON RT APU ACCESS DOOR 5TH FRAME FROM FWD END, FRAME HAD 100% MATERIAL LOSS AND IS OUT OF LIMITS, IAW B767 SRM 52-40-02-1A. FABRICATD NEW FRAME, IAW BOEING DWG 148T6557 REV- AND B767 SRM 51-40-05. INSTALLED NEW FRAME, IAW B767 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FLOOR BEAM STA 615-632 AND BETWEEN RBL 33-24 HAS CORROSION ON LOWER SURFACE. UPON THE EVALUATION OF FLOOR BEAM AT STA 615-632 BETWEEN RBL 24-33 THE CORROSION ON THE 'L' ANGLES 2 EA WERE FOUND CORRODED WITH 100% MATERIAL LOSS, IAW B767 SRM 51-10-02. FABRICATED AND INSTALLED NEW 'L' ANGLES 2 EA ONTO THE FLOOR BEAM, IAW B767 SRM 51-40-02 AND B767 SRM 51-70-12-0G-0.

Part: STRINGER SPLICE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPT BILGE AREA FS 430 STRINGER 36L SPLICE HAS LIGHT CORROSION. REMOVED 5 EA RIVETS TO GET ACCESS AND REMOVED CORROSION AT STA 430 STR 36L, IAW B767 SRM 51-40-02 & 51-10-02. PERFORMED NDT ORIGINAL MATERIAL .032, MATERIAL LOSS .004, REMAINING MATERIAL .028 FOUND OUT OF LIMITS, IAW B767 SRM 53-00-03 ASSET NR 0017630. REMOVED AND FABRICATED SPLICE FROM PN BAC1498-202 7075-T6 PO NR FS2007003 DIM. 11 1/4", IAW B767 SRM 53-30-03-2R-2. APPLIED PROTECTIVE FINISHES, IAW B767 SRM 51-20-01.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 91,312 hrs · 26,458 cycles

FWD CARGO DOOR SKIN HAS 2 EA DENTS ALONG THE 2 LOWER MOST BEAMS THAT ARE OUT OF LIMITS AND MUST BE REPAIRED. REPAIRED FWD CARGO DOOR SKIN, IAW EA 20025 REV IR.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, POSSIBLE CORROSION ON SHEAR TIE, AFT SIDE OF STA 742 WEB BETWEEN STR 33R-34R. REMOVED CORROSION FROM SHEAR TIE STA 742 STR 33R-34R AND FOUND OUT OF LIMITS, IAW B767 SRM 51-10-02. REMOVED AND REPLACED SHEAR TIE, IAW BOEING DWG 140T2102 REV D FR.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, CORROSION ON SHEAR TIE STA 742 AFT SIDE OF WEB BETWEEN STR 34R-35R. REMOVED AND INSTALLED NEW SHEAR TIE PN: 140T2102U203 P/O FS2006975 AT FWD CARGO BILGE AREA STA 742 AFT SIDE OF WEB BETWEEN STR 34R-35R, IAW B767 SRM 51-40-02 AND BOEING DWG 143T1513 REV -.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPARTMENT BILEGE AREA FS 412 FRAME SHEAR-TIE HAS LIGHT CORROSION BETWEEN STRINGER 33R-34R. REMOVED CORROSION AT FWD CARGO COMPARTMENT SHEAR-TIE STA 412 BETWEEN STR 33R-34R FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-1. REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE, IAW B767 SRM 51-40-02-06-0 AND DWG 141T1224 REV AC, H.

Part: STRINGER SPLICE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT PIT STRINGER SPLICE HAS EXFOLIATED CORROSION ON BOTH SIDES AND BULGING SKIN STA 1307 35L. UPON EVALUATION OF STR 35L AND SPLICE AT SAT 1307, FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 35L, IAW B767 SRM 53-00-03-2R-2.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 91,312 hrs · 26,458 cycles

SHEAR TIE CORRODED, FWD CARGO BILGE, STA 566 BETWEEN S37L-S36L. REMOVED CORROSION FROM SHEAR TIE STA 566 STR 37L-36L AND FOUND IN LIMITS, IAW B767 SRM 53-00-07-1A-1. RESTORED PROTECTIVE FINISHES, IAW B767 SRM 51-21-01.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

LT OVERWING FILLER PORT ADAPTER CUTOUT FAYING SURFACE AT WING UPPER AND LOWER SKIN IS CORRODED. REMOVED CORROSION FROM LT OVERWING FILL PORT AND FOUND OUT OF LIMITS, IAW B767 SRM 57-20-01-1A-1. REPAIRED LT OVERWING FILL PORT, IAW FAS EA 20026 REV IR. TOPCOAT TO BE APPLIED ON Q2031 PAINT TASK.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT PIT CARGO FLOOR SUPPORT EXFOLIATED STA 1263 LBL 24. REMOVED AND EVALUATED AFT CARGO FLOOR SUPPORT AT STA 1263 LBL 24 FOUND OUT OF LIMITS WITH 100% MATERIAL LOSS. FABRICATED NEW AND INSTALLED FLOOR SUPPORT, IAW B767 SRM 51-10-02, 51-40-02 AND DWG 96F5667847 REV B.

Part: STRINGER — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT OF FWD CARGO PIT STA 774 STR 36R HAS 5 SQ IN EXFOLIATED CORROSION AND CRACKED. STR 36R STA 774, FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 36R, IAW B767 SRM 53-00-03-2R-2.

Part: SHEAR TIE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT CARGO COMPARTMENT BILGE AREA HAS CORRODED SHEAR TIE AT BS 1175 BL 0. SHEAR TIE AT STA 1175 BL 0 FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-2. REMOVED AND REPLACED SHEAR TIE, IAW BOEING DWG 140T2102 REV FR C.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, SHEAR TIE CORRODED STA 522 BETWEEN S38R-37R. REMOVED CORROSION FROM SHEAR TIE STA 522 STR.38R-37R AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-2. REMOVED AND REPLACED SHEAR TIE, IAW B767 SRM 51-40-02-0G-0, BOEING DWG 143T1204 REV D. CIC TO BE APPLIED ON TASK NR 6753A852PT1-6.

Part: WEB — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO WEB AT STA 522-588 INBOARD OF STRAP HAS CORROSION IN VARIOUS PLACES. REMOVED THE CORROSION FROM THE WEB AT STA 522-588 AND FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-02. FABRICATED AND INSTALLED NEW WEB, IAW B767 SRM 51-40-02 AND B767 SRM 53-30-01.

Part: FITTING — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

AFT OF FWD CARGO PIT STA 774 STR 39L HAS 5 SQUARE IN EXFOLIATED CORROSION. EVALUATED STR 39L, SPLICE AND CHANNEL FITTINGS 2 EA STA 784-754 AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REMOVED AND REPLACED STR 39L SECTION, SPLICE AND 2 EA CHANNEL FITTINGS STA 754-784, IAW B767 SRM 53-00-03-2R-2, BOEING DWG. 140T0128 REV D. RESTORED PROTECTIVE FINISHES, IAW B767 SRM 51-20-01.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD PIT CORROSION UNDER NUTPLATE LOWER SIDE OF WEB 566-588 RBL 4. REMOVED AND EVALUATED FWD CARGO INTERCOSTAL AT STA 566-588 RBL 4 AND FOUND OUT OF LIMITS, IAW B767 SRM 51-10-02. FABRICATED NEW AND INSTALLED INSTERCOSTAL, IAW B767 SRM 51-40-02 AND 53-30-53.

Part: LINER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

DURING OPEN OF BULK CARGO DOOR INNER LINER FOUND EXFOLIATED CORROSION ON INNER SKIN LOWER SECTION. REMOVED AND REPLACED THE BULK CARGO DOOR DUE TO EXFOLIATED CORROSION ON THE INNER SKIN, IAW B767 AMM 52-36-01.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, CORROSION ON SHEAR TIE ST 724 AFT SIDE OF WEB BETWEEN S37R-38R. REMOVED CORROSION AT SHEAR TIE ON FWD CARGO COMPARTMENT STA 742 BETWEEN S37R-38R FOUND 100% OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-2. REMOVED AND REPLACED, IAW B767 SRM 51-40-02-0G-0 AND DWG 143T1214 REV E NEW PN 140T2102U252 PO FS2006994.

Part: STRINGER SPLICE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO RT SIDEWALL, STRINGER SPLICE HAS CORROSION AT STA 434 S29R. EVALUATED FWD CARGO COMPARTMENT STRING SPLICE AT STA 434 STR 29R FOUND 100% OUT OF LIMITS, IAW B767 SRM 53-00-03. REMOVED, LOCATED AND DRILLED AND INSTALL NEW SPLICE PN 140T0115U2 PO FS2007092, IAW B767 SRM 51-40-02-0G-0 AND B767 SRM 51-40-05.

Part: WEB — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO STA 632 RBL 37-43 CORROSION ON THE OUTBOARD SIDE FWD FACE OF THE WEB. REMOVED CORROSION FROM WEB AT STA 632 RBL 37-43 AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-51-1A-1. REPAIRED WEB, IAW B767 SRM 53-00-07-2R-3.

Part: DOUBLER — CORRODED (BULK CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

UPON REMOVAL OF Z-STIFFNER AT BULK CARGO THRESHOLD, FOUND DOUBLER AT AFT SIDE OF FRAME 1417 CORRODED. REMOVED AND REPLACED THE CORRODED DOUBLER AT THE AFT SIDE OF THE FRAME AT STA 1417 STR 32L-34L, IAW FAS EA 20031 REV R.

Part: FAIRING — DAMAGED (RT WING TO BODY) · airframe 91,312 hrs · 26,458 cycles

RT WING TO BODY FAIRING STA 1065 RBL 15 HAD ELONGATED HOLES AND GOUGE ON SCREW HOLE. REPAIRED HOLE AT STA 1081 37R-38R, IAW FAS EA 20032 REV IR.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA SHEAR TIE HAS CORROSION UNDER IT, STA 698 BETWEEN S36L-37L. SHEAR TIE AT STA 698 STR36L-37L FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO BILGE AREA, CORROSION ON SHEAR TIE AFT SIDE STA 742 BETWEEN S33L-32L. FOUND CORRODED AREA ON FWD CARGO BILGE AREA SHEAR TIE STA 742 BETWEEN STR 33L TO 32L WITH MATERIAL LOSS 100% TO BE OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-2. REMOVED AND INSTALLED NEW SHEAR TIE P/N 140T2102-227 P/O FS2006954, IAW B767 SRM 51-40-02 AND DWG 143T1214 REV E.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPARTMENT BILGE AREA HAS CORRODED SHEAR TIE AT BS 654 LBL 6. REMOVED AND REPLACED FWD CARGO SHEAR TIE STA 654 LBL 6, IAW B767 SRM 51-40-02, BOEING DWG 143T1210 REV D.

Part: SHEAR TIE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

FWD CARGO COMPARTMENT BILGE AREA STA 412 SHEAR TIE HAS CORROSION BETWEEN STR 34R-35R. REMOVED CORROSION AT FWD CARGO COMPARTMENT SHEAR TIE STA 412 BETWEEN STR 34R-35R FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-2. REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE, IAW B767 SRM 51-40-02-0G-0 AND DWG 141T1224 REV AC H.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 91,312 hrs · 26,458 cycles

REF DMI 127742 LP 1158798. CORROSION DAMAGE ON SKIN PANEL (P/N 146T3230-1) NEAR STA 1329, S-35L-CATEGORY-C TIME LIMITED REPAIR CW PART 3 OF EO 6753A851 PERMANENT REPAIR. COMPLIED WITH INSTALLATION OF PERMANENT REPAIR AT STA 1324-1460 STR 33L-39L, PER PART 3 OF ATLAS EO 6753A851PT3 REV 2.

Part: RIVET — PULLED (FUSELAGE) · airframe 91,206 hrs · 26,390 cycles

DURING WALKAROUND, PILOT FOUND A "PULLED THROUGH" RIVET ON THE IN FUSELAGE ABOVE AND AFT OF THE CABIN PRESSURE OUTFLOW VALVE.(<P>REF LOGPAGE 1157429, ITEM# 20 FOR PERMANENT REPAIR IAW EO # 6753A871. REF LOGPAGE 1157428 ITEM #18 FOR HFEC INSPECTION M15, DMI # 127742 CLEARED.</P><P>LOGPAGE 1157429: REPAIRED AREA IAW B767 SRM 53-00-01-2R-1 REPAIR 1. DMI NO. 127742 CLEARED.&NBSP;IAW ATLAS EO NO. 6751A871 REV. 0 PERMANENT REPAIR.&NBSP;</P>)

Part: SKIN — DELAMINATED (BS 434) · airframe 91,219 hrs · 26,397 cycles

FOUND METAL DELAMINATION FORWARD OF FWD EQUIPMENT EXHAUST VALVE. REPAIRED AREA IAW SRM 53-00-01-2R-1 REPAIR 1 AND EO 6753A871 REV 6 PERMANENT REPAIR.

Part: MODULE — LEAKING (TE FLAP) · airframe 90,397 hrs · 25,839 cycles

ITEM 1: LEFT HYDRAULIC SYSTEM EICAS MESSAGE QTY ON, AFTER GEAR UP. LOSS OF INDICATION VALVE, PRESSURE WAS 3000+. ITEM 2: CENTER HYDRAULIC SYSTEM EICAS MESSAGE QTY CAME ON AFTER GEAR UP. QTY WAS +-50. PRESSURE WAS 200. T/S PER FIM 29-11 FT 831, FOUND MONITOR UNIT HYD READINGS FALSE. REMOVED AND REPLACED HYD QTY MONITOR UNIT IAW AMM 29-33-01. OPS CHECK GOOD. (P/N OFF: 367-027-006, S/N OFF: 356) LP 1084354 - ITEM 2: FOUND TE FLAP MODULE ASSY LEAKING IN RT WHEEL. REMOVED AND REPLACED IAW AMM 27-51-32-44-027. OPS AND LEAK CHECK GOOD. SERVICED CTR HYD IAW 12-12-01.

Part: TUBE — CRACKED (NR 2 ENG TURBINE) · airframe 90,057 hrs · 25,663 cycles

#2 ENGINE TURBINE SECTION COOLING TUBE, 8:00 POSITION HAS A 1 IN CRACK AT PREVIOUS WELD.&NBSP;(<P>REMOVED AND REPLACED #2 ENGINE TURBINE SECTION COOLING TUBE IAW B767 AMM 75-24-08.</P>)

Part: FASTENER — CORRODED (PT7 PROBE) · airframe 90,057 hrs · 25,663 cycles

#2 ENGINE TURBINE SECTION 6 EA PT7 PROBES ATTACH HARDWARE CORRODED. DOT 127-046.(<P>CLEANED #2 ENGINE TURBINE SECTION PT7 PROBE ATTACH HARDWARE IAW B767 SOPM 20-30-03 AND AMM 77-21-02.</P>)

Part: STIFFENER — CORRODED (BS 786) · corrosion level 2 · airframe 90,057 hrs · 25,663 cycles

KEEL BEAM, R/H O/B STIFFENER AT STA 786 BULKHEAD HAS CORROSION.&NBSP;(<P>REMOVED SPLICE FITTING (STIFFENER), FABRICATED, AND INSTALLED NEW SPLICE (STIFFENER) P/N 7075T651. .500 BARE PLATE, PO #1904679 DIM (3.6' X 14.2") AT KEEL BEAM R/H STA 786 BULKHEAD IAW B767 DWG 143T2200 REV "E".</P>)

Part: CONNECTOR — DAMAGED (NR 1 IDG) · airframe 90,057 hrs · 25,663 cycles

ENGINE #1 IDG ELEC PLUG D00412 HAS DAMAGED BACKSHELL.&NBSP;(<P>REMOVED AND REPLACED #1 ENGINE IDG PLUG D00412 IAW B767 WDM 24-11-11 AND PERFORMED A GOOD OPS CHECK IAW B767 AMM 24-11-00.</P>)

Part: STARTER — INOPERATIVE (APU) · airframe 90,057 hrs · 25,663 cycles

APU STARTER IS INOP.&NBSP;(<P>REMOVED AND REPLACED APU STARTER ASSY IAW B767 AMM 49-41-01. PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 49-41-01. NO DEFECTS NOTED.</P>)

Part: INERTIA REEL — UNSECURE (CABIN) · airframe 89,312 hrs · 25,229 cycles

DURING PREFLIGHT NOTICED ONE INERTIAL REEL LATCH NOT SECURED. OPENED COVER & RESECURED LATCH AND 2 INERTIAL REELS FELL OUT. INSTALLED 2 DESCENT DEVICES IAW 25-61-03.

Part: DUCT — DAMAGED (LEFT) · airframe 89,097 hrs · 25,064 cycles

LEFT DUCT LEAK EICAS AT 3000 FT MSL. FOLLOWING QRH PROCEDURE, LIGHT REMAINED ILLUMINATED. LIGHT WENT OUT APPROXIMATELY 5 MINUTES LATER. REMOVED AND REPLACED A DAMAGED LEFT CROSSOVER DUCT ASSEMBLY IAW 36-11-01-404-064-006, LEAK AND OPS CHECKED GOOD.

Part: BLADE — NICKED (ENGINE FAN) · airframe 88,773 hrs · 24,800 cycles

NR 1 & 40 BLADES FOUND NICKED. BLENDED WITHIN LIMITS IAW AMM 72-31-02. PERFORMED A DYE PENETRANT INSPECTION ON THE BLADES AT BLENDS. NO CRACKS FOUND, COMPLETED FPI IAW MM 70-11-06, OK FOR SERVICE.

Part: SHEAR TIE — CORRODED (BS 1087) · airframe 88,605 hrs · 24,685 cycles

CORROSION ON SHEAR TIE AT BS 1087, STRINGER 37L. REPLACED THE SHEAR TIE IAW DWG 146T1201.

Part: FAILSAFE — CRACKED · airframe 88,605 hrs · 24,685 cycles

FOUND A CRACK INDICATION IN THE FAILSAFE STRAP. REPAIRED IAW EO 6753A070, REV 10, AND SB 767-53A0100, REV 3.

Part: ANGLE — CRACKED (NLG WW) · airframe 88,605 hrs · 24,685 cycles

DURING AN HFEC INSPECTION OF THE NOSE WHEEL WELL VERTICAL ANGLES. FOUND A 1 INCH CRACK INDICATION. REPAIRED THE ANGLE IAW SRM 51-70-12, AND EO 6753A027, REV 10, PAGE 6, STEP 6.

Part: FAILSAFE — CRACKED · airframe 88,605 hrs · 24,685 cycles

FOUND CRACK INDICATION IN THE FAILSAFE STRAP AT LOWER FASTENER HOLE IAW EO 6753A070 REV.10 PART 2, STEP 8, AND SB 767-53A0100 REV 3 AD 2012-09-04. REPAIRED IAW EO 6753A070, REV 10 AND SB 767-53A0100 REV 3.

Part: SPINNER — CRACKED (NR 1 ENGINE) · airframe 88,147 hrs · 24,365 cycles

ON WALKAROUND, FOUND NR 1 ENGINE SPINNER CAP CRACKED ON SEVERAL OF THE FLANGE SURFACES&NBSP;(<P>REMOVED AND REPLACED FORWARD SPINNER CAP IAW B767 AMM 72-51-01 TORQUE CHECKS GOOD&NBSP;</P>)

Part: DUCT — FAILED (CABIN AIR) · airframe 88,146 hrs · 24,364 cycles

LOUD BANG AT FL190 FOLLOWING BY CENTER BODY LEAK EICAS AND LOSS OF PRESSURIZATION. REMOVED AND REPLACED AIR DUCT IN THE AFT CARGO BAY BS 1065 TO 1241 AND LEAK CHECKED GOOD IAW AMM 36-11-00.

Part: PDU — FAILED (SLAT SYSTEM) · airframe 87,925 hrs · 24,211 cycles

LEADING EDGE SLAT ASYMMETRY AFTER TAKE OFF. REMOVED AND REPLACED LEADING EDGE SLAT PDU IAW TASK 27-81-10-024-001, OPS CHECKED NORMAL, NO FAULTS NOTED. REMOVED AND REPLACED PSEU BOX IAW AMM 32-09-03.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 87,566 hrs · 23,946 cycles

UPON LEVEL OFF AT FL 360, RT ENG COMPRESSOR STALLED 4 TIMES. NO EXCEEDANCES WERE NOTED. ACCOMPLISHED NR 2 ENG BORESCOPE INSPECTION IAW ECM ITEM NR 2016-098 STEPS 4-9, WITH NO SIGNIFICANT DISCREPANCIES NOTED. REFERENCE WO 012864 FOR DETAILS. ACCOMPLISHED STEPS 1 - 3 & 12-13 OF ECM 2016P-098, NO DEFECTS NOTED AT THIS TIME. R & R NR 2 ENG EVBC IAW AMM 75-31-01,PN 776555-7, SN A3222. PERFORMED LEAK CHECK, OPERATIONS CHECK & RIG IAW 75-31-01.L R & R NR 2 ENG FCU, PN 773333-21, SN F1485 IAW AMM 73-21-01, LEAK & OPERATIONS CHECK OK. R & R NR 2 ENG FUEL PUMP, PN 715001-49, SN 3224 IAW AMM 73-11-01. LEAK & OPERATIONS CHECKED OK.

Part: DOOR — MISSING (AC BAY) · airframe 87,527 hrs · 23,918 cycles

DURING CLIMB OUT AT 17000 FT, VIBRATION FELT IN AIRFRAME, NO ABNORMAL INDICATION OR EICAS MSG. SLOWED ACFT TO 270, LEVELED AT 18000 FT, POST FLT FOUND RT PACK DOOR MISSING & LT PACK DOOR DAMAGED.

Part: UNKNOWN — NOT REPORTED (RT ENGINE) · airframe 87,525 hrs · 23,917 cycles

IN CRUISE AT FL 350, THE RT ENG COMPRESSOR STALLED AT LEAST 3 TIMES. WE REDUCED POWER & CONTINUED. NO ADDITIONAL STALL AT REDUCED POWER. PERFORMED TEST IAW AMM 71-01-00, PERFORMED MINOR ADJUSTMENTS. COMPLIED WITH TEST 10 & 9 WITHIN TEST 8. NO ADJUSTMENTS NEEDED FOR TEST 10, MINOR ADJUSTMENTS MADE WITHIN TEST 9. AFTER ADJUSTMENTS INDICATIONS WERE NORMAL. PERFORMED BORESCOPE INSPECTION STAGES 5, 8 & 15, NO DISCREPANCIES NOTED IAW AMM 72-00-00 601.

Part: ESCAPE ROPE — DAMAGED (CABIN) · airframe 87,407 hrs · 23,848 cycles

MAIN DECK DESCENT DEVICE DAMAGED, PN 379103D-29 & SN 12059. R & R DESCENT DEVICE IAW AMM 25-61-03.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 86,647 hrs · 23,368 cycles

DENT IN LOWER SKIN SURFACE ON LT HORIZONTAL STAB AT AUXILIARY SPAR STATION 333, 7.25". ACCOMPLISHED SKIN REPAIR IAW SRM 51-70-10 IAW SRM 55-10-01 FIG 101.

Part: CABLE — UNSECURE (NR 1 ENGINE) · airframe 86,613 hrs · 23,335 cycles

BLOCK TURN BACK DUE TO LT THRUST LEVER BINDING. FOUND LT FEEDBACK CABLE ON NR 1 ENG UNSECURED REF MDDR LT REV INOPERATIVE. SECURED CABLE, ENG RUNS IAW AMM 71-00-00. OPERATIONS CHECKED NORMAL, THRUST LEVER TRAVEL VERIFIED, OK FOR SERVICE.

Part: INDICATOR — NOT SEATED (ENTRY DOOR) · airframe 8,619 hrs · 22,873 cycles

LEFT FWD ENTRY DOOR EICAS ALERT MSG RECEIVED IN FLIGHT. FOUND POSITION FLAG ON DOOR NOT FULLY SEATED JUST BELOW DOOR HANDLE. INSPECTED & CYCLED DOOR SEVERAL TIMES, NO DEFECTS NOTED IAW AMM 52-11-00-715-128.

Part: FIRE BOTTLE — DISCHARGED (NR 2) · airframe 8,559 hrs · 22,208 cycles

LOWER DECK NR 2 FIRE EXTINGUISHER BOTTLE SHOWS DISCHARGE. TRANSFERRED TO DMI 46541 MEL 26-23-01-01.

Part: ENGINE — VIBRATION (LEFT) · airframe 85,592 hrs · 22,255 cycles

SIGNIFICANT VIBRATION LT ENGINE ALL RANGE OF RPM. REPAIRED IAW SOPM 20-20-01 AND 20-41-02.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 85,512 hrs · 22,170 cycles

FLAPS REMAIN AT 5 AFTER FLAP HANDLE COMMAND TO 1, T/E FLAP DISAGREE LIGHT ILLUMINATED. STAB TRIM LIGHT ILLUMINATE WHENEVER TRIM SWITCH " PILOTS YOKE IS TRIMED, 3- LT ENG GEN DRIVE LIGHT ILLUMINATED, DISCONNECTED GEN DRIVE, A/T WILL NOT ENGAGE. 5- L/E SLAT EDGE SLAT DISAGREE / LIGHT ILLUMINATED. OPEN

Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 84,884 hrs · 21,748 cycles

ON PUSHBACK, RT HYD DEMAND PUMP SHOWED 0 PRESSURE. PERFORMED INSPECTION CHECK OF RT HYD ACMP, PULLED AND RESET THE L-16, R & R SYS HYD PRESSURE CIRCUIT BREAKER, OPS CHECKED NORMAL. REF AMM 29-11-01, OK FOR CONTINUED SERVICE.

Part: ACTUATOR — SEPARATED (SPOILER) · airframe 84,674 hrs · 21,645 cycles

LEFT WING TRAILING FLAP DAMAGE, DUE TO SPOILER PANEL ACTUATOR SEPARATED. ACCOMPLISHED EO 6757A040, PART NR 1. TEMP REPAIR.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE) · airframe 84,644 hrs · 21,619 cycles

AFTER ENGINE START, EICAS WARNING MESSAGE "RT ENG EEC PROBE", AND "ENG MACH PROBE" ILLUMINATED.