N762CK

Part: FIRE LOOP — WARNING MESSAGE (ZONE 400) · airframe 96,145 hrs · 30,717 cycles

DURING INSPECTION, RIGHT ENG FIRE LOOP 1 STATUS MESSAGE. DEFERRED R ENG FIRE LOOP 1 IAW MEL 26-11-1-1. MAINTENANCE PROCEDURES CW. PLACARD INSTALLED. AC REMAINS NO ETOPS. MBCB 12/21/25

Part: WINDOW — CRACKED (ZONE 200) · airframe 95,830 hrs · 30,529 cycles

DURING CLIMB, R1 WINDOW HEAT EICAS WITH WINDOW CRACKING.. AIRCRAFT RETURNED TO CVG. (ATB). MTX GROUNDED AC . REMOVED AND REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER IAW B767 AMM 56-11-01 AND B767 AMM 30-41-01 OPS CHECK GOOD MTX RETURNED AC TO SERVICE.

Part: START VALVE — INOPERATIVE (ZONE 400 RT) · airframe 95,660 hrs · 30,437 cycles

ON TAXI, RT ENGINE START VALVE INOP. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-80-00-2-1. REMOVED AND REPLACED RT ENGINE START VALVE. DI 64875 CLEARED. A/C REMAINS NO ETOPS IAW B767 AMM 80-11-02. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — FAULTED (ZONE 700) · airframe 95,546 hrs · 30,378 cycles

ANTI-SKID MSG AFTER PUSHBACK AND ENGINE START. *#8 XCDR SYSTEM FAULT* AIRCRAFT RETURNED TO BLOCKS. (BTB) MAINTENANCE DEFERRED IAW MEL C ABX-32-42-1-1A. AIRCRAFT RETURNED TO SERVICE.

Part: IDG — FAULTED (NR 2 GENERATOR) · airframe 95,131 hrs · 30,165 cycles

DURING TAXI OUT AFTER ENGINE START, EICAS MESSAGE APPEARED RT GENERATOR OFF. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE IDG IAW MEL ABX-24-00-1-1. MBCB 04/03/25. PLACARD INSTALLED, MAINTENANCE ACTION C/W. AIRCRAFT REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

Part: ACTUATOR — LEAKING (ZONE 600 SPOILER) · airframe 95,081 hrs · 30,136 cycles

DURING TAXI AFTER START RH HYDRAULIC QUANTITY EICAS MSG. QUANTITY ON STATUS PAGE 0.22. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. INSPECTED AND FOUND #11 OUTBOARD SPOILER PCA LEAKING . REMOVED AND REPLACED #11 PCA IAW B767 AMM 27-61-02, OPS CHECK GOOD , C/W RII 27-26-1. MTX RETURNED A/C TO SERVICE .

Part: SMOKE DETECTOR — MALFUNCTIONED (ZONE 200) · airframe 95,006 hrs · 30,091 cycles

MAIN DECK FIRE INDICATION AND SMELL OF SMOKE ON FLT DECK DURING DE-ICING , CREW DECLARED EMERGENCY AND CALL FIRE RESCUE , AND (QRH) PERFORMED EVACUATION PROCEEDURE. MTX GROUNDED AC AND AFTER ALL WAS SAFE. MTX RETURNED A/C TO NORMAL CONFIG FROM QRH NNC 8.36. REF LP 38954-19/2, 38954-19/3, AND 38954-21/1 FOR OTHER FINDINGS AND WORK PERFORMED. PERF L&R ENG IDLE RUNS PER AMM TASK 71-00-00-735-034-H00, PERF LH / RH PACK OPS CK PER AMM TASK 21-00-00-862-024. ALL OPS CKS GOOD, NO FIRE WARNINGS, FOUND NO EVIDENCE OF FIRE, AND NO SMELL OF SMOKE PRESENT. SMOKE DETECTOR 8 ON MAIN DECK SHOWING INDICATION FOR THE A LOOP .REMOVED AND REPLACED CARGO SMOKE DET M09803 IAW B767 AMM IAI TASK 26-14-01-424-001. OPS CHECK GOOD. A/C REMAINS NO ETOPS. FOUND NO EVIDENCE OF FIRE OR SMOKE RETURNED AC TO SERVICE

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 94,993 hrs · 30,085 cycles

ON BLOCK OUT L ENG A/I VALVE FAILED TO OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C .MTX MANUALLY ACTUATED VALVE ,THEN OPS CHECKS WERE GOOD IAW B767 AMM 30-21-03. A/C REMAINS NO ETOPS. AND MTX RETURENED AC TO SERVICE.

Part: BLEED AIR SYS — FAULTED (APU) · airframe 94,946 hrs · 30,061 cycles

DURING TAXI WHILE STARTING ENGINE APU DOES NOT HAVE PNEUMATIC AIR FOR ENGINE START,A/C THEN RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED APU AIR FOR DEPARTURE IAW MEL ABX-49-11-1-1. AND RETURNED A/C TO SERVICE. A/C DEPARTED

Part: VALVE — WARNING MESSAGE · airframe 94,879 hrs · 30,029 cycles

FWD EQPT VAL YELLOW MESSAGE APPEARED WHILE ENTERING RUNWAY FOR TAKEOFF. QRH PROCEDURES DID NOT REMEDY.AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT , MTX DEFERRED THE FWD EQUIPT. VALVE IAW MEL ABX-21-58-8-1-1. AND RETURNED AC TO SERVICE.

Part: IRU — MALFUNCTIONED (ZONE 100) · airframe 94,859 hrs · 30,018 cycles

DURING TAXI THE CTR IRU FAIL APPEARED , AC RETURNED TO THE GATE (BTB) MTX GROUNDED AC AND MTX REMOVED AND REPLACED CENTER IRU UNIT IAW AMM 34-21-00 OPS CHECK GOOD A/C DOWNGRADED CAT I PENDING TEST 30-40 MTX RETURNED AC TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE) · airframe 94,841 hrs · 30,008 cycles

DUING TAXI AFTER ENGINE START L ENG.ANTI ICE AND VALVE LIGHT ILLUMINATED AC RETURNED TO GATE(BTB) MTX GROUNDED AC MTX MANUALLY ACTUATED VALVE AND PERFORMED OPS TEST IAW B767 AMM 30-21-03. OPS TEST GOOD AND RETURNED AC TO SERVICE .

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYS) · airframe 94,782 hrs · 29,979 cycles

DURING CLIME OUT LE SLAT DISAGREE LIGHT CAME ON ,AC RETURNED TO FIELD (ATB) AND MAINTENACE GROUNDED AC , MTX T/S IAW KAC FIM 27-51 FT 809. FSEU SHOWS NO EXISITING FAULTS. FAUTL HISTORY SHOWS LVR1 NOT IN DETENT. OS CHECKED IAW KAC AMM 27-81-00. OPS CHECK GOOD AT THIS TIME. AND RETURNED AC TO SERVICE AND AC DEPARTED

Part: WARNING MESSAGE — ILLUMINATED (CABIN TEMP) · airframe 94,538 hrs · 29,824 cycles

DURING PUSHBACK FWD CABIN TEMP EICAS MSG AC RETURNED TO BLOCK AND MTX GROUNDED AC . DEFERRED FOR DEPARTURE IAW MEL ABX-21-61-6-2 . AND RETURNED AC TO SERVICE AND DEPARTED

Part: KEELBEAM — DAMAGED (ZONE 100) · corrosion level 2 · airframe 94,443 hrs · 29,770 cycles

WHILE 762CK WAS UNDERGOING C-CHECK IN OSC, MAINTENANCE DISCOVERED DAMAGE TO THE KEEL BEAM HORIZONTAL WEB AT STA 860 AND BL 0. AFTER DAMAGE REMOVAL, THE REMAINING MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMITS OFSRM 53-50-12, ADI, FIGURE IOI. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF/ A/, WHICH IS AN FAA-DER APPROVED REPAIR.DURINGTHE CURRENT MAINTENANCE CHECK OF THE DATUM AIRCRAFT, DURING EXTERNAL GVI INSPECTIONS, A DAMAGE WAS FOUND ON THE HORIZONTAL WEB KEEL BEAM AREA STA 860 -BL0. REWORK AREA, NOMINAL THICKNESS 0.080" PER BOEING DRAWING 145T8612, REMAINING MATERIAL 0.046", 42.5% MATERIAL REINOVED. REPAIRED IAW FLIGHT VEHICLES CONSULTING ENG. CONTROL # 24108 REV IR ABD ABX-REA-5350-65484-00 AC RETURNED TO SERVCE

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,443 hrs · 29,770 cycles

"WHILE 762CK WAS UNDERGOING C-CHECK IN OSC, MAINTENANCE FOUND CORROSION ON THE FRAME WEB AT STA 1307, BETWEEN S-371 & S-381 ATLBL 11. CORROSION REMOVAL EXCEEDED THE LIMITS GIVEN IN SRM 53-00-07, AD 1, FIGURE IO I. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF/ A/, WHICH IS AN FAA-DER APPROVED REPAIR .DURING THE CURRENT MAINTENANCE CHECK OF THE DATUM AIRCRAFT, DURING EXTERNAL GVI INSPECTIONS, A CORROSION WAS FOUND AT FRAME WEB LOCATED AT STA 1307, BETWEEN S-37L AND S-38L- LBL 11. THE DAMAGE WAS REMOVED, AND THE WEB HAS BEEN INSPECTED PER NOT HFEC SURFACE WITH NO DAMAGE NOTE. THE WEB IS 7075-T6 0.032"" CHEM MILLED TO MIN OF 0.025"". THE THICKNESS OF THE WEB AT THE CUTOUT IS 0.032"". REPAIRED IAW FLIGHT VEHICLES CONSULTING INC.EO #24108-4 REV IRAND ABX-REA-5360-65517-00 AC RETURNED TO SERVICE "

Part: SWITCH — OUT OF POSITION · airframe 94,443 hrs · 29,771 cycles

POST C-CHECK MAINTENANCE EVALUATION FLIGHT. CLIMBING THROUGH 10,000' VMO POINTER/BARBER POLE FAILED TO INCREASE SPEED TURNED OFF A/T TO CONTROL SPEED. AIRCRAFT PERFORMED AN AIR TURN BACK (ATB). AIRCRAFT WAS GROUNDED. FOUND VMO/MMO SWITCH IN ALT POSITION MOVED SWITCH TO THE NORMAL POSITION IAW B767 AMM 32-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 94,443 hrs · 29,770 cycles

WHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. AFTER CORROSION REMOVAL, THE REMAINING MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMITS OF SRM 57-20-0 I AD I, FIGURE 10 I. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/, WHICH IS AN FAA-DER APPROVED REPAIR. DURING MAINTENANCE C4 IN OSC , UH WING UPPER SKIN UPPER SURFACE CORROSION WAS FOUND AT STA 1066 AT FWD SPAR. CORROSION REMOVED BLENDED AREA TO A 20 TO 1 TAPER MATERIAL LOSS WAS 0.034" -NOMINAL THICKNESS OF 0.200". BLEND OUT MAPPED WITH A 0.500" GRID. REPAIRED IAW FLIGHT VEHICLES CONSULTING ENG. CONTROL # 24108-2 REV IR AND ABX REA -5720-65485-00 AC RETURNED TO SERVCE

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 94,443 hrs · 29,770 cycles

WHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. AFTER CORROSION REMOVAL, THE REMAINING MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMITS OF SRM 57-20-0 I AD I, FIGURE 10 I. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/, WHICH IS AN FAA-DER APPROVED REPAIR. , UH WING UPPER SKIN UPPER SURFACE CORROSION WAS FOUND AT STA 1066 AT FWD SPAR. CORROSION REMOVED BLENDED AREA TO A 20 TO 1 TAPER MATERIAL LOSS WAS 0.034" -NOMINAL THICKNESS OF 0.200". BLEND OUT MAPPED WITH A 0.500" GRID. REPAIRED IAW FLIGHT VEHICLES CONSULTING ENGINEERING ORDER CONTROL #24108-2 REV IR AND ABX-REA-5720-65485-00. AC RETURNED TO SERVCE

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 94,416 hrs · 29,750 cycles

DURING TAXI BULK CARGO DOOR INDICATION UPON STARTING #2 ENGINE . AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC. OPENED AND CLOSED BULK CARGO DOOR MULTIPLE TIMES TO VERIFY OPERATION IAW B767 AMM 52-36-01 OPS CHECK GOOD DOOR INDICATING CLOSED IN COCKPIT. RETURNED AC TO SERVICE .AND DEPARTED

Part: HOSE — BROKEN (HYD SYSTEM) · airframe 94,118 hrs · 29,579 cycles

ON TAXI OUT GOT EICAS MESAGE L HYD QTY FOLLOWINED BY CAUTION BEEPER EICAS MESSAGE L HYD SYSTEM PRESS. STATUS PAGE SHOWED L HYD QTY 0.17 RF. FOUND BROKEN / DAMAGED HOSE FROM RUDDER RATIO CHANGER (REF LEAK CODE 320-6-3 LEFT TO PCA HOSE ASSY). REPLACED PER AMM 20-10-10 WITH FLEX LINE . NO LEAKS NOTED. LH HYD SYS IS SERVISE TO FULL . DEFERRED FLEX LINE PER MX TRACKING PER GMM 07.04 PERFORMED REINSPECTION EVERY DAY. PLACARD INSTALLED MBCB NEXT C-CHECK. FLEX LINE WAS R&R WITH RUD CONTROL RAIO CHANGE HOSE IAW AMM 27-21-15. LEAK CHECK GOOD PLACARDS REMOVED. CLEARS DI 50561.

Part: COMPUTER — MALFUNCTIONED (ZONE 300) · airframe 93,317 hrs · 29,021 cycles

AFTER ENGINE START, WE HAD AN ELEV FEEL STATUS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED ELEVATOR FEEL COMPUTER PER B767 AMM 27-31-00. LEAK CHECK GOOD. OPS CHECK GOOD PER B767 AMM 27-31-00. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,245 hrs · 28,974 cycles

RUDDER TRIM INDICATOR INOPERATIVE ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE . MAINTENANCE DEFERRED IAW MEL 27-21-3. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,245 hrs · 28,974 cycles

LT HYDRAULIC QUANTITY DROPPING DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED AIRCRAFT FOR HYDRAULIC LEAKS. NO EXTERNAL LEAKS NOTED. SUMPED FUEL FROM LH MAIN DUE TO RECENT MX. NO HYD FLUID NOTICED IN SAMPLE. RESERVICED HYD (LH) TO FULL. REF B767-2A/B. AC REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,182 hrs · 28,921 cycles

TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED AFTER FLAPS 5 WERE SELECTED & INDICATED 5. MISSED THE APPROACH AND PERFORMED TROUBLESHOOTING & QRH PROCEDURES. DUE TO THE COMBINATION OF MAINTENANCE ISSUES, AN EMERGENCY WAS DECLARED DUE TO LANDING DISTANCE & STOPPING CONCERNS AND AN UNEVENTFUL LANDING WAS PERFORMED. AIRCRAFT WAS GROUNDED BY MAINTENANCE. PERFORMED FLAP + SLAT DETAILED VISUAL INSPECTION WITH FLAPS EXTENDED. NO DAMAGES NOTED. OPERATED FLAPS ELECTRONICALLY REF AMM 27-51-00 OPS CHECKS NORMAL. PERFORMED FSEU BITE PER FIM 27-57-00 FT 810. NO FAULTS DISPLAYED. OPERATED FLAPS + SLATS WITH HYD PUMPS CHECK OBSERVED SLOW FROM1-5 BUT WORKING PROPERLY WITH ADP ON, CYCLED FLAPS/SLATS SEVERAL TIMES NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,033 hrs · 28,835 cycles

AUTO THROTTLES DISCONNECTED ON TAKE OFF ROLL. LOW SPEED ABORT. AIRCRAFT EXITED RUNWAY AND CONTACTED MAINTENANCE CONTROL. AUTO THROTTLE SYSTEM WAS DEFERRED BY THE CREW PER MEL 22-30-1A. AIRCRAFT RETURNED TO SERVICE.

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 92,721 hrs · 28,714 cycles

AFT CABIN TEMP INOP LIGHT ON DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE C/W CABIN TEMP SENSOR FILTER CLEANING PER AMM 21-51-00. OPS CHECK OF AFT CABIN TEMP CHECKS ON GRD. C/W BITE CHECK OF CABIN TEMP. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOTHROTTLE SYS — FAULT MESSAGE · airframe 92,601 hrs · 92,601 cycles

ON TAKEOFF ROLL AFTER (THR) SELECTED EICAS MSG AUTO THROTTLE DISC DISPLAYED. AIRCRAFT EXITED ON TO TAXI WAY AND AUTO THROTTLE SYSTEM WAS DEFFERED BY FLIGHT CREW. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 92,592 hrs · 28,618 cycles

LOW SPEED ABORT LESS THAN 70 KIAS AUTO THROT DISC ANNUCIATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AUTO THROTTLE SYSTEM IAW MEL 22-30-1A. AIRCRAFT RETURNED TO SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOTHROTTLE SYS) · airframe 92,546 hrs · 28,597 cycles

A/T DISC ON LOW SPEED TAKE OFF, TAKE OFF ABORTED. FLIGHT CREW DEFERRED 22-30-1A. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENCE. MAINTENANCE CHECKED MCDP FAILURES. DID NOT FIND ANY FAILURES ON LEG 02, LEG 18 HAD A/T DISC TMC 310801. NO OTHER RELATED FAILURES. RAN MCDP TEST 02 HAD NO INFC TMC A/T WARN -1 NRM, NO INFC TMC A/T WARN-1 BAT, AND NO INFC TMC PLA POS R. TEST 10 PASS, TEST 30 FAILED SAME AS TEST 02. DI REMAINS, DEACTIVATION PROCEDURES APPLIED. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 92,159 hrs · 28,428 cycles

C HYDRAULIC PRIMARY 2 PUMP DID NOT COME BACK ON AFTER ENG START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE C 2 HYDRAULIC PUMP IAW MEL 29-11-2. PLACARD INSTALLED, AIRCRAFT RETURNED TO SERVICE.

Part: WEB — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

TORQUE BOX WEB AT STA 610 RBL 44 SHOWS EVIDENCE OF CORROSION

Part: WEB — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

FWD CARGO FLOOR WEB AT STA 610 RBL 38 HAS EVIDENCE OF CORROSION

Part: WEB — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

EVIDENCE OF CORROSION ON FLOOR WEB AT STA 1280 RBL 44

Part: WEB — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

EVIDENCE OF CORROSION ON TORQUE BOX WEB AT STA 1290 RBL 40

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

AFT CARGO DOOR SURROUND APPROX. STA 1280 APPROX. RBL 43 TORQUE BOX FRAME LOWER CHORD CORRODED

Part: WEB — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

FWD CARGO FLOOR WEB AT STA 566 RBL 32 HAS EVIDENCE OF CORROSION

Part: STIFFENER — CRACKED · airframe 92,004 hrs · 28,360 cycles

LEFT WING I/B AILERON O/B CLOSURE RIB WEB HAS EVIDENCE OF CHAFFING

Part: TORQUE BOX — CORRODED · corrosion level 2 · airframe 92,004 hrs · 28,360 cycles

CORROSION IN AFT PIT ON UPPER SURFACE OF TORQUE BOX CLOSEOUT AT APPROX. STA 1280 LBL 20

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 90,711 hrs · 27,631 cycles

LE SLAT DISAGREE. PERFORMED FLAP SLAT ELECTRONIC UNIT BITE AND FOUND FAULT CODE 27-51104 TRAILING EDGE DISAGREE INTERMITTENT. RESET FAULT. PERFORMED OPERATIONS CHECK OF LEADING EDGE FLAPS/SLATS THROUGH FULL CYCLES IN NORMAL MODE. ALL CHECKS GOOD REFERENCE FAULT ISOLATION MANUAL 27-51 FAULT TREE 809 AND AMM 27-51-00

Part: GUIDE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 90,429 hrs · 27,445 cycles

FORWARD CARGO COMPARTMENT, MIDDLE AUXILLIARY SIDE GUIDE RAIL IS CORRODED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,429 hrs · 27,445 cycles

L313 EMERGENCY LIGHT DOORWAY WILL NOT ILLUMINATE.

Part: STIFFENER — CRACKED (BS 242) · airframe 88,029 hrs · 26,376 cycles

VERTICAL STIFFENER ON FORWARD SIDE OF STA 242 FLOOR BEAM AT LBL 30 HAS EVIDENCE OF CRACK

Part: DOOR FRAME — CORRODED (BS 1486) · corrosion level 2 · airframe 88,029 hrs · 26,376 cycles

R2 DOOR FRAME HAS CORROSION AT STA 1486 WL 206 ON INNER SURFACE

Part: ESCAPE ROPE — FRAYED (COCKPIT) · airframe 86,194 hrs · 25,148 cycles

CAPTAINS ESCAPE ROPE IS FRAYING.

Part: CLAMP — DISCONNECTED (GROUND SERVICE) · airframe 86,383 hrs · 25,207 cycles

CABIN ALTITUDE DISPLAYED. FOUND GROUND SERVICE AC CONNECTION DUCT CLAMP DISCONNECTED. CONNECTED IAW AMM 20-11-00. LEAK CHECKED GOOD. PRESSURIZED AIRCRAFT AND FOUND TO BE SATISFACTORY.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 86,289 hrs · 25,178 cycles

SMOKE IN COCKPIT FROM GLARE SHIELD VENTILATION DUCT. PERFORMED ENGINE RUNS IAW B-767 AMM 71-00-00 AND B-767 FIM 21-00 TASK 801,ALL CHECKS GOOD. PERFORMED ENGINE INSPECTION FOR OIL,HYDRAULIC FUEL LEAKS PER B-767 AMM 71-7-00. ALL CHECKS GOOD. PERFORMED INSPECTION CHECK OF AIRCRAFT PACK SYSTEM IAW B-767 AMM 21-51-00 ALL CHECKS GOOD. FOUND RIGHT HAND HYDRAULIC SYSTEM QUANTITY AT 1.29, TRANSFERRED HYDRAULIC FLUID TO "C" SYSTEM IAW B-767 AMM 12-12-01. NOTE: OVER-SERVICED HYDRAULIC SYSTEM CAN CAUSE SMOKE IN THE COCKPIT. PERFORMED REPAIR CONFIRMATION DURING ENGINE RUNS IAW B-767 AMM 21-00-21 AND B-767 FIM 21-00 TASK 801. ALL CHECKS GOOD. PERFORMED GENERAL WIRING INSPECTION OF MAIN AND FORWARD ELECTRONICS COMPARTMENT IAW BSWPM 20-10-06 ALL SYSTEM TESTS/CHECKS NORMAL AT THIS TIME.

Part: WEB — CORRODED (BS 1263) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

AFT PIT BALLMAT FLOOR SUPPORT WEB CORRODED AT STA 1263

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

LEFT WING NR 1 OTBD FLAP SUPPORT FITTING TOP BOLT HOLE CORRODED.

Part: WEB — DAMAGED (BS 588) · airframe 86,194 hrs · 25,148 cycles

UPPER WEB OF TORQUE BOX HAS SEVERAL AREAS OF DAMAGE AT BS 588 BETWEEN LBL 20 AND RBL 20

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

SHEAR TIE CORRODED IN FWD CARGO BAY AT BS 742, LBL 39.

Part: STRINGER — CORRODED (BS 1307) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

STRINGER 2R CORRODED AT BS 1307.

Part: SUPPORT RIB — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

LEFT WING NR 1 FLAP SUPPORT OUTBOARD SUPPORT RIB HAS CORROSION IN BORE FOR ACTUATOR BOLT

Part: WEB — CORRODED (BS 544) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON TORQUE BOX UPPER WEB IN THE FWD CARGO BAY, BS 544, LBL 14

Part: LUG — WORN (NR 1 NACELLE) · airframe 86,194 hrs · 25,148 cycles

NR 1 PYLON LOWER SPAR FITTING, LUG HOLE WORN

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

LEFT WING NR 2 FLAP SUPPORT FITTING HAS CORROSION IN FOUR BOLT HOLES.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

BULK CARGO DOOR INNER LOWER LIP HAS EVIDENCE OF CORROSION.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

LT WING I/B MAIN FLAP INNER MID SPAR LOWER CORD CORRODED.

Part: STRINGER — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

RT SIDE HORIZONTAL STABILIZER HAS CORROSION ON STRINGER 4 LOWER I/B END.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

HORIZONTAL STAB TORSION BOX COMPARTMENT RT SIDE, UPPER AREA STR 8 HAS CORROSION.

Part: STRINGER — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

RT SIDE HORIZONTAL STABILIZER HAS CORROSION ON STRINGER 8 LOWER I/B END.

Part: STRINGER — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

RT SIDE HORIZONTAL STABILIZER HAS CORROSION ON STRINGER 7 LOWER I/B END.

Part: STRINGER — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

RT SIDE HORIZONTAL SECTION OF STAB TORSION BOX STRINGER 10 CORRODED I/B END OF STRINGER.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

FRAME OUTER CHORD AT STA 1043 BETWEEN S-11R AND S-12R IS CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD STA 1373 LBL 25 TO RBL 10.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

FWD CARGO COMPARTMENT STA 522 APPROXIMATELY STR 39R TOP OF TORQUE BOX STRUCTURE HAS EVIDENCE OF CORROSION.

Part: MOUNT FITTING — CRACKED (NR 2 PYLON) · airframe 86,194 hrs · 25,148 cycles

NR 2 PYLON STRUT INBD SIDE APPROX NS 205 INBD MOUNT FOR THE FAN COWL SUPPORT BEAM IS CRACKED ON AFT SIDE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON UPPER CHORD OF STA 1219 FRAME RBL 21 TO RBL 48, AFT PIT.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION OF FRAME UPPER CHORD AT STA 1197 +44 RBL 21 TO RBL 40.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD STA 1197 +132 RBL 21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD STA 1197 RBL 20 TO 44.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD AT STA 1197 +88 LBL 34 TO 42.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD STA 1197 +22 RBL 20 TO 43.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON UPPER CHORD OF STA 1219 FRAME LBL 24 AND 39, AFT PIT.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

FAIL SAFE CORD AT STA 1021 IS CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

LT FUSELAGE FRAME STA 1131 STRINGER 8L FRAME WEB CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON LBL 41 STA 1197 +110 ON LOWER SIDE OF FRAME.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION AT STA 1197 +88 RBL 43 FRAME UPPER CHORD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON FRAME UPPER CHORD STA 1197 +66 RBL 21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION UNDER NUT PLATES AT STA 1153 RBL 28 TO LBL 38.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,194 hrs · 25,148 cycles

CORROSION ON LOWER SIDE OF UPPER CHORD OF STA 1197 +66 LBL 19 TO 39.