N364CM

Part: SENSOR — DEFECTIVE (N1 SPEED) · airframe 100,868 hrs · 37,472 cycles

DURING TAXI, RIGHT ENGINE N1 STARTED ON 2 STARTS AND NO N1 INDICATION ON SEI SHOWS 0. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED N1 SPEED SENSOR IAW B767 AMM 77-12-01. OPS CHECK GOOD. A/C REMAINS ETOPS 180. STANDBY INDICATOR REINSTALLED IAW B767 AMM 77-41-01. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE GOGGLES — CRACKED (ZONE 200) · airframe 100,735 hrs · 37,421 cycles

DURING INSPECTION, MAINTENANCE FOUND SMOKE GOGGLE CRACKED AT SUPERNUMERARY MID SEAT. REMOVED AND REPLACED SMOKE GOGGLE AT SUPERNUMERARY MID SEAT PER REF. AMM 25-64-00. AIRCRAFT RETURNED TO SERVICE.

Part: CDU — ODOR (ZONE 200) · airframe 100,604 hrs · 37,367 cycles

ON CLIMBOUT, THERE WAS A STRONG ODOR OF ELECTRIC WIRE BURNING. EMERGENCY DECLARED. AIR TURN BACK (ATB) TO CVG. REF LP 39228-63/3 & 39228-65/2 FOR TROUBLESHOOTING & WORK PERFORMED. NO DEFECTS NOTED. LP 39228-63/3 PERFORMED INSPECTION OF ALL C/BS & PACK BAYS. PERFORMED HIGH POWER ENG RUNS IAW AMM 71-00-00. PERFORMED 05-51-56 INSPECTION IAW AMM WHICH INCLUDES AMM 21-00-21. REMOVAL OF OIL CONTAMINATION AT PACK. PNEUMATIC SYSTEM, NO ODORS. LP 39228-65/2 INSPECTED MEC FOR ELECTRICAL BURNING OR ODOR PER AMM 20-66-04, NO DEFECTS. OPS LT & RT PACKS INSPECTED FOR ODOR OR ELECTRICAL BURNING PER AMM 21-51-00, NO DEFECTS. OPS CHK & INSPECTION OF FLT DECK LIGHT INDICATORS PER AMM 33-13-00, NO DEFECTS. INSPECTED & OPS CHK ALL FLT DECK WINDOW WIRING & HEAT SYS PER AMM 30-41-00, NO DEFECTS. INSPECTED LAV, GALLEY, & HOT CUP PER AMM 25-41-00 AND 25-31-00. NO DEFECTS. CHKD CAPT / FO'S FOOT / SHOULDER HEATERS PER AMM 21-45-11, NO DEFECTS. OPS CHKD WXR SYS PER AMM 34-43-00, NO DEFECTS. INSPECTED LT & RT CU'S PER AMM 34-61-02, NO DEFECTS. PER MC REQUEST R & R CDU IAW AMM 34-61-02, OPS CHECKED GOOD. ACCOMPLISHED EVAL FLT PER M-281. NO DEFECTS NOTED. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.

Part: FMC — INTERMITTENT (ZONE 200) · airframe 100,551 hrs · 37,346 cycles

ON TAXI OUT, RIGHT FMC MOMENTARILY BLANKED. A/C RETURNED TO BLOCKS. (BTB). DEFERRED IAW MEL C ABX-34-61-1-1A. REMOVED AND REPLACED R FMC IAW B767 AMM 34-61-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 300 RUDDER) · airframe 100,236 hrs · 37,223 cycles

ON TAXI, RUDDER RATIO ON EICAS MSG., ALL HYDRAULIC PRESSURES NORMAL. AIRCRAFT RETURNED TO BLOCKS. (BTB) ACCOMPLISHED OPERATIONAL TEST OF RUDDER AND RUDER TRIM CONT IAW AMM 27-21-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: START VALVE — DEFECTIVE (ZONE 400) · airframe 100,051 hrs · 37,154 cycles

DURING PUSHBACK, #2 ENGINE RIGHT ENGINE STARTER VALVE INOP. AIRCRAFT RETURNED TO BLOCKS. (BTB) . DEFERRED IAW MEL C ABX-80-00-2-1. REPLACED RH ENGINE START VALVE IAW AMM 80-11-02 / 401. DI 63480 REMAINS OPEN DUE OPS CHECK PENDING. RH ENG START VALVE OPS CHECKED GOOD ON ENG RUN PER B767 AMM 71-00-00. DI CLEARED, PLACARD PULLED. AIRCRAFT RETURNED TO SERVICE AND A/C REMAINS NO ETOPS.

Part: ENGINE — POWER LOSS (LEFT) · airframe 99,854 hrs · 37,058 cycles

ABORTED TAKEOFF (ATO) SLIGHTLY UNDER 80 KTS. RT ENGINE MADE TO POWER, HOWEVER, LT ENGINE ONLY MADE IT TO 88% N1. AIRCRAFT RETURNED TO BLOCKS. (BTB). RAN ENGINES AT TAKEOFF POWER WITH EEC'S OFF, ENGINES MADE TAKEOFF POWER IAW 71-00-00, ITEM TRANSFERRED TO DI# 61889 AS PER MEL 73-21-1-1B, MBCB 5/10/25, PLACARD INSTALLED AIRCRAFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: HEATER — MALFUNCTIONED (PITOT HEAD) · airframe 99,387 hrs · 36,850 cycles

AFTER PUSHBACK CAPT PITOT DISCREET LIGHT ILLUMINATED W/ EICAS MSG A/C RETURNED TO GATE(BTB) AND MTX GROUNDED AC MTX PERF FIM 30-31 FT 805 WITH PITOT HT BREAKER PULLED (CAPT) AND TEST SWITCH HELD WARMING LIGHT NEVER ILLUMINATES, VERIFIED NO POWER TO K241 CURRENT SENSING RELAY. PIN C1, VERIFIED GOOD 115VAC TO PROBE, JUMPERED A&B PINS ON D1010 115 VAC NOW PRESENT TO K241. PER WOM 30-31-11REMOVED AND REPLACED CAPT PITOT PROBE LH UPPER PER AMM 34-11-01. H7CK GOOD PER AMM 30-31-00. LOW RANGE AND HIGH RANGE LEAK CK GOOD PER AMM 34-11-00, PERF L&R ENG RUNS PER AMM 71-00-00, L7REMAINS EXTINGUISHED NO EICAS MSG. A/C REMAINS RVSM COMPLIANT. AC RELEASED ETOPS 180 . AC RETURNED TO SERVICE

Part: FMC — ODOR (COCKPIT) · airframe 99,360 hrs · 36,840 cycles

DURING MAINTENANCE PRE FLIGHT THE F/O FMC CDU BURN SMELL AND C/B P11 E29 POP OUT. MTX GROUNDED AC DEFERRED PER MEL 34-61-1-1A MX PROCED C/W PLACARD INSTALLED A/C RELIESED NO ETOPS .VERIFIED WARN ELEX STATIS MSG.NOT IN VIEW SEE LOG 39126-13/1 FOR ABX REA-3060-65654-00 DEFERRAL .C/W'D ABX--REA-3460-65654-00 FOR TRACKING IAW GMM CH1,SECTION 07.04 AC RELEASED NO ETOPS PLACARD ROTATED PLACARD INSTALLED . MTX RETURED AC TO SERVICE .

Part: WARNING LIGHT — ILLUMINATED (ZONE 800) · airframe 99,308 hrs · 36,814 cycles

DURING CLIMB MAIN CARGO DOOR LIGHT ON AT 30.0' AND EXSTINGUISHED AT 20.0' AC RETURND TO FIELD (ATB) AND LANED MTX GROUNDED AC.MTX DEFERRED MAIN CARGO INDICATION FOR DEPARTURE IAW MEL-ABX-52-71-1-2 . AND RETURNED AC TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 100) · airframe 99,176 hrs · 36,759 cycles

DURING TAXI OUT C HYD PRIMARY 1 EICAS MESSAGE APPEARED , AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . TROUBLESHOT, AND REMOVED AND REPLACED ELECTRICAL LOAD CONTROL UNIT IAW B767 AMM 29-11-14 OPS CHECK OK AT THIS TIME . AND RETURNED AC TO SERVICE .

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 99,152 hrs · 36,747 cycles

ABORTED TAKE-OFF AT ~75KTS DUE TO WARNING HORNING, RED FLAPS EICAS MESSAGE. AC ABORTED T/O DURING ABORT AFTER EXPENDING, SPOILERS, NOTED REF SPOILER EICAS MESSAGE AFTER ABORT WHILE TAXING NOTED FLAP/SLAT ELEC STATUS MTX GROUNDED AC . UPON INSPECTION FOUND NO ACTIVE STS MSG. CK'D MCDP + FOUND NO LATCHED MSG. T/S PER FIM 27-51 FAULT TREE 836. NO DEFECTS NOTED. PFM FSEU BITE TEST IAW AMM 27-51-01. TEST PASS NO DEFECTS NOTED. AC RETURNED TO SERVICE

Part: PNEUMATIC SYSTEM — FAULTED (APU) · airframe 99,029 hrs · 36,696 cycles

DURING TAXI THERE WERE NO APU PNEUMATICS. ACFT RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED APU. PNEUMATICS FOR DEPARTURE IAW MEL ABX-49-11-1-1 AND RETURNED AC TO SERVICE .

Part: PIN — NO DISCREPANCY (ZONE 700) · airframe 98,929 hrs · 36,652 cycles

ON PUSH OUT TOW BAR LOCK SNAPED DUE TO BYPASS PIN NOT INSTALLED AC RETURNED TO GATE AND MTX GROUNDED AC AND COMPLIED WITH INSPECTION OF THE NLG IAW B767 AMM 05-51-29 AND NO DAMAGE NOTED .MTX RETURNED AC TO SERVICE

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 98,724 hrs · 36,569 cycles

RH ENGINE LOW OIL UPON ENGINE START AND PUSH.BACK LH 19 ON START DROPPED TO 18 THEN TO 13 AND STABLE AT 14. RH 21 THEN 17 ON IDLE, NO ISSUES. AC RETURNED TO GATE AND MTX GROUNDED AC MTX CHECKED OIL @ SIGHT GLASS, FULL. EICAS READING 19 LH + 21 RH. SERVICED LH ENG W 1QT OIL. EICAS READING 20 + 21. OIL STILL IN SIGHTGLASS. WORK IAW B767-2A.AND RETURNED AC TO SERVICE

Part: FMC — FAILED (LEFT) · airframe 98,713 hrs · 36,564 cycles

ON ROLL OUT TO TAKEOFF LEFT FMC FAIL EICAS MESSAGE DISPLAYED , AC ABORTED TAKE OFF AND TAXIED OFF RUNWAY , THEY PERFORMED QHR AND PERFORMED A FLIGHT CREW DEFFERRAL IAW MEL ABX-34-61-1-1A. AND AC DEPARTED .

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 98,679 hrs · 36,538 cycles

DURING MAINTENANCE CHECK DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20- 01) AT RH UPPER WING SKIN AT WING STRINGER U-2 TO U-4 AND RUNS UNDER THE RIB CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THE FASTENER HOLES OF THE RIB CHORD. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.108" INCHES FROM INITIAL THICKNESS OF 0.208", INCH (UT MEASURED) WITH MATERIAL LOSS OF 0.100", INCH, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, ADL 1, TABLE I OF 0.030 INCHES (BASED ON 0.196-INCH UT READING). THE THICKNESS PER DRAWING IS 0.192 INCHES REPAIRED IAW ABX-REA-5725-65330-00 AND FVCI EO 24126-2 REV A AC RETURNED TO SERVICE

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 98,678 hrs · 36,538 cycles

"DURING MAINTENANCE CHECK AT PEMCO (TPA) AND DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20-01) AT RH UPPER WING SKIN AT WINGS STRINGER S-15 AND RUNS UNDER THE PLUS CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THE FASTENER HOLES OF THE PLUS CORD. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.126¿ INCHES FROM INITIAL THICKNESS OF 0.172¿, INCH (UT MEASURED) WITH MATERIAL LOSS OF 0.046¿, INCH, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, ADL 1, TABLE I OF 0.030 INCHES (BASED ON 0.180-INCH UT READING). THE THICKNESS PER DRAWING IS 0.172¿ INCHES REPAIRED IAW FVCI EO 24126-3 REV IR AND ABX-REA-5725-65329-00. AC RETURNED TO SERVICE "

Part: APU — AUTO SHUTDOWN (ZONE 100) · airframe 98,586 hrs · 36,501 cycles

APU SHUT DOWN AFTER AC LEFT THE BLOCK AC RETUREN TO BLOCKS AND MAINTENANCE GROUNDED AC AND DEFERRED THE APU IAW 49-11-1B AND RETURNED TO SERVICE AND AC DEPARTED .

Part: CONTROL PANEL — FAULTED (FLT DIRECTOR) · airframe 98,586 hrs · 36,501 cycles

CREW DISCREPANCY: CAPT FD NOT SHOWING SELECTED ALTITUDE, ALSO NOT SHOWING TO AND FD AT TOP OF PFD. WENT BACK TO BLOCK. REMOVED AND REPALCED MCP PER AMM 22-11-02. OPS CK GOOD PER AMM 22-00-02, MCDP TEST NO. 4 A/C REMAINS CAT I PENDING MCDP TEST 30/40 SEE LP 38609-73/3 REURNED AC TO SERVICE

Part: INDICATOR — FAULTED (FLT DIRECTOR) · airframe 98,586 hrs · 36,501 cycles

LOST FLIGHT DIRECTOR DURING PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED ACFT AND TRANSFERED POWER FD CAME BACK C/W MCDP GROUND TEST 30 IAW AMM 22-00-01. ALL INDICATIONS NORMAL A/C REMAINS CAT 3B OPERATIONAL RETURNED AC TO SERVICE

Part: APU — AUTO SHUTDOWN (ZONE 100) · airframe 98,584 hrs · 36,500 cycles

APU SHUT DOWN DURING PUSH, AC RETURUNED TO GATE AND MANTENANCE GROUNDED AC AND DEFERRED APU FOR FLIGHT IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE AC DEPARTED

Part: DOOR — UNSECURE (MAIN CARGO) · airframe 98,146 hrs · 36,313 cycles

MCD WARNING ANNUCIATORS INDICATOR ILLUMINATED DURING PUSH-BACK , AC RETURED TO THE GATE AND MAINTENANCE CLOSED AND LATCHED MAIN CARGO DOOR IAW B767 AMM 52-32-00 DOOR OPS CHECK GOOD .AC TAXIED OUT AND DEPARTED IN SERVICABE CONDITION ,.

Part: APU — SHUTDOWN · airframe 98,095 hrs · 36,291 cycles

APU SHUTDOWN ON PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC . AND DEFERRRED THE APU FOR DEPARTURE IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE. AC DEPARTED

Part: FSEU — FAULTED (FLAP/SLATS) · airframe 98,015 hrs · 36,257 cycles

DURING ILS 31R AT KJFK, WHEN FLAPS SELECTED TO 25, FLAPS STAYED AT 20. EXECUTED MISSED APPROACH. HELD AT CHANT. DECLARED AN EMERGENCY. REBRIEFED AND COMPLETED VISUAL APPROACH TO 31L. LANDED SAFELY.C/W FSEU BYTE CHECK I/A/W FIM27-51 FT 809. NO FAULTS. INSPECTED OVERLOAD TRIP INDICATORS, NO FAULTS FOUND. CYCLED FLAPS 4X I/A/W AMM 27-51-00. FULL RANGE OP'S CHECK GOOD. REF M1A 38760-75 FOR FURTHER T/S REMOVED AND REPLACED FSEU I/A/W AMM 27-51-01. OPERATED FLAPS I/A/W AMM 27-51-00. OP'S CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 97,741 hrs · 36,136 cycles

CAPT FD INOP AND ALT IND ON A/S INOP .A/C RETURNED TO GATE MAINTENANCE GROUNDED A/C .C/W TURNING OFF FLIGHT DIRECTOR AND COMPLETE IRU REALIGNMENT PER AMM 34-24-01  OPS CHECK GOOD ON CAPT'S AND FO'S FLIGHT DIRECTOR  A/C REMAINS CAT IIIB STATUS.MAINTENANCE RETURNED TO SERVICE AND A/C DISPATCHED.

Part: PITOT TUBE — MALFUNCTIONED (ZONE 200) · airframe 97,721 hrs · 36,125 cycles

L AUX PITOT EICAS AND OVERHEAD DISCREATE LT ILLUMINATED AFTER ENGINE STARTED AC RETURNED TO BLOCK AND MAINTENACE GROUNDED AC .T/S FIM PER 30-31 FT. 804, FOUND PITOT FAULTY, REPLACED L AUX PITOT PROBE IAW AMM 34-11-01, PART EFFECTIVITY VERIFIEDPERFORMED L AUX PITOT/STATIC LEAK CHECK FOUND F/O STATIC LEAK OVER LIMITS . PER AMM 34-11-00 .REMOVED AND REPLACED ELBOW LEADING FROM HARD LINE TO FLEX LINE PERFORMED PITOT STATIC HIGH RANGE LEAK CHECK IAW AMM 34-11-00 NO LEAKS NOTED.REMOVED AND REPLACED R/H AIR DATA COMPUTER PER B767 AMM 34-12-00. PART EFFECTIVITY VERIFIED. PERFORMED LEAK CHECK AND OPS CHECK OF THE R/H ADC IAW AMM 34-12-01 CKD NORMAL.AC RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,903 hrs · 32,829 cycles

RIGHT CENTER FUEL PUMP INOP, CENTER RT PUMP DID NO OPERATE AFTER START OF RIGHT A/C RETURNED TO BLOCK AND MAINTENANCE GROUNDED A/C.DEFERRED SYSTEM IAW MEL 28-22-2A. FOR DISPATCH . AC FLOWN TO LIM . PERFORMED GROUND FAULT INTERRUPTOR OPS TEST. FOUND RELAY K10696 POPPED. UPON RESET OF RELAY PUMP STILL INOP. (LOW PRESS LIGHT) PER AMM 28-22-00. DI #46402 REMAINS OPEN PERFORMED REACTIVATION OF RIGHT CENTER FUEL PUMP IAW MEL 28-22-2A. OPS CHECK GOOD IAW AMM 28-22-00. THIS CLEARS DI 46402. ACFT REMAINS ETOPS 180. PLACARDS REMOVED. AC RETURNED TO SERVICE

Part: MODULE — LEAKING (SLAT SYS) · airframe 97,405 hrs · 35,985 cycles

AFTER TAKEOFF EICAS MSG 1) CHYD QTY 2)C HYD 2 OVHT CENTER HYD SYSTEM REAAD 0.16 AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT GROUNDED BY MAINTENANCE. TROUBLE SHOT AND FOUND OUTBOARD SLAT PDU CONTROL VALVE MODULE LEAKING .REMOVED AND REPLACED LEFT OUTBOARD SLAT PDU CONTROL VALVE MODULE IAW AMM 27-81-12 SERVICED HYDRAULICS AND RETURNED A/C TO SERVICE .

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 97,367 hrs · 35,968 cycles

AFTER ENGINE START, CAPT'S AIRSPEED AND ALTITUDE INDICATIONS WERE BLANK. CAPT'S & F/O'S FD'S WERE ALSO BLANK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. NO EICAS OR STATUS MESSAGES DISCREPANCY STARTED AFTER GPU POWER TRANSFER. GPU HAS AN ELECTRICAL SURGE, CHANGED GPU, PERFORMED RIGHT ENGINE START AT THE GATE AND POWER TRANSFER WAS SUCCESSFUL. OPS CHECK SATISFACTORY AT THIS TIME. A/C REMAINS NO ETOPS.AC RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 97,188 hrs · 35,897 cycles

MN CARGO DOOR LIGHT ILLUMINATED WHILE CLIMBING THRU 5000 FT RAN QRH RETURNED TO KLAX THE LIGHT DISTINGUISHED AFTER 10 MINS AT 7000 LEVEL FLIGHT GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED DOOR INDICATION IAW MEL-52-71-1-2 AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTED (MEC) · airframe 96,966 hrs · 35,815 cycles

FWD EQUIPMENT SUPPLY VALVES DO NOT AGREE, EICAS MSG FWD EQUIPMENT VALVE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED AIR SUPPLY MODULE ASSY. IAW B767 AMM 36-23-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,838 hrs · 35,761 cycles

EMERGENCY LIGHTS FLICKERING OFF AND ON WITH LIGHTS ARMED DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED EMERGENCY LIGHTING IAW MEL 33-51-1C. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,802 hrs · 35,746 cycles

ON TAXI OUT R HYD. LEVEL WAS INDICATING 0.74 RF. RETURNED TO GATE. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE SERVICED R HYD SYSTEM TO 1.10 IAW B767 AMM 12-12-01. NO LEAKS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,679 hrs · 35,696 cycles

C HYD PRIM 1 EICAS MESSAGE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED A VISUAL AND FUNCTIONAL CHECK OF THE C1 PUMP SHOWED ALL NORMAL. LOAD TEST AND INDICATIONS NORMAL. NO ISSUES NOTED WITH OPERATION. ALL WORK REF B767 AMM 29-11-00. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,197 hrs · 35,517 cycles

AFTER ENGINE START AUTO SPEED BRAKE APPEARED ON EICAS AND AUTO SPD BRK LIGHT ILLUMINATED ON OVERHEAD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE AUTO SPEEDBRAKE SYSTEM IAW MEL 27-62-1A. MAINTENANCE PROCEDURES COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 95,931 hrs · 35,431 cycles

ON PUSH BACK MAIN CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED DOOR SWITCH AND LIGHT EXTINGUISHED. DOOR VERIFIED LOCKED IAW B767 AMM 52-32-22. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — LOW PRESSURE (HYD SYSTEM) · airframe 95,535 hrs · 35,297 cycles

L HYD ACMP HAS LOW PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED L ACMP PER AMM 29-11-01 LEAK CHK OK. AIRCRAFT RETURNED TO SERVICE

Part: AOA — FAULT MESSAGE · airframe 95,101 hrs · 35,164 cycles

LH AOA PROBE ON TAXI OUT, AIRCRAFT TO BLOCK AND GROUNDED BY MAINTRNANCE. MAINTENANCE RESET AOA CIRCUIT BREAKER OPS CHECK NORMAL IAW B767 AMM 30-32-00. AIRCRAFT RETURNED TO SERVICE

Part: CONTROL VALVE — FAULTED (LT A/C PACK) · airframe 94,871 hrs · 35,082 cycles

LH PACK OVERHEAT AND INCREASING TEMP PERFORMED QRH NO HELP. AICRAFT ATB TO CVG AND WAS GROUNDED BY MAINTENANCE. INSPECTED MEL PROCEDURES FOR DI 34798 PROPER MEL PROCEDURES WERE IN PLACE. INSPECTED HEAT EXCHANGERS AND ALL DUCTS FOR BLOCKAGE OR LEAKS NO DEFECTS. CHECKED TRIM AIR SUPPLY CHECK VALVE FOR HEAT ON RH SIDE NO DEFECTS. REMOVED AND REPLACED LH PACK FLOW CONT/SOV PER B767 AMM 21-51-01 OPS/LEAK NORMAL. RE-APPLIED MEL 21-51-2 AC IS NO ETOP. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 94,701 hrs · 35,017 cycles

DURING AIRCRAFT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE RIGHT WING TOP SKIN PANEL NO. 2 (112T3302-4) UPPER SURFACE AT THE FWD SPAR FASTENER LINE AT WS 225. CORROSION WAS REMOVED BY BLENDING AND MINIMUM REMAINING THICKNESS DOCUMENTED IN 0.50” X 0.50” GRID MAPPINGS. THE REMAINING THICKNESSES WERE OUT OF LIMITS PER SRM 57-20-01, REQUIRING A DOUBLER TO BE INSTALLED ON THE UPPER SKIN SURFACE. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE ABOVE NOTED CONDITION, AS APPROVED BY FVCI 8110-3. REPAIRED PER ABX-REA-5725-64378-00.

Part: UNKNOWN — CORRODED (ZONE 200) · corrosion level 2 · airframe 94,701 hrs · 35,017 cycles

DURING AIRCRAFT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL UPPER OUTER CHORD(143T8204-1). THE 2 AREAS OF CORROSION ARE LOCATED AT STA 566 AND STA 610. AREA 1 AT STA 566- ORIGINAL MATERIAL .200 INCH, MATERIAL LOSS OF .059 INCH, MIN REMAINING THICKNESS .141 INCH. AREA 2 AT STA 610- ORIGINAL MATERIAL .200 INCH, MATERIAL LOSS OF .067 INCH, MIN REMAINING THICKNESS .133 INCH. CORROSION WAS REMOVED BY BLENDING PER 767-300 SRM 51-10-02 AND THE LOSS OF MATERIAL WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER 767-300 SRM 53-00-15. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE NOTED CONDITION AS APPROVED BY FVCI 8110-3. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 94,701 hrs · 35,017 cycles

DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE RIGHT WING TOP SKIN PANEL NO. 2 (112T3302-4) UPPER SURFACE AT THE FWD SPAR FASTENER LINE. FOUR LOCATIONS OF CORROSION REPORTED OUT OF LIMITS PER 767-300 SRM 57-20-01. LOCATIONS #1, #2 AND #4 ARE REPAIRED BY THIS REA. LOCATION #3 REQUIRES A DOUBLER REPAIR AND IS ACCOMPLISHED BY ABX-REA 64378. CORROSION WAS REMOVED BY BLENDING AND MINIMUM REMAINING THICKNESS DOCUMENTED IN 0.50” X 0.50” GRID MAPPINGS. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE ABOVE NOTED CONDITION, AS APPROVED BY FVCI 8110-3. REPAIRED COMPLETED PER ABX-REA-5725-64376-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR.

Part: BEAM — CRACKED (ZONE 200) · airframe 94,701 hrs · 35,017 cycles

AMES NR 0496 - CABIN, STA 903.5 RBL89, RH INNER CHORD(STUB BEAM) TRANSITION RADIUS CRACKED(END MARKED). STUB BEAM REPAIRED PER ABX-EA-5300-0052-101 (REPAIR - INNER CHORD, STA 903.5, RBL89, B767). VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR

Part: NONE — NONE (ZONE 100) · airframe 94,691 hrs · 35,014 cycles

WARNING ELEX STATUS MSG ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R&R STALL WARNING CARD IAW B767 AMM 27-32-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 94,397 hrs · 34,921 cycles

AUTOTHROTTLES DID NOT ADVANCE TO N1 POWERSETTING FOR TAKE-OFF. ABORTED TAKE OFF AT 40 KTS AND RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE RESET THE AUTO-THROTTLE COMPUTER CIRCUIT BREAKERS. PERFORMED MCDP AUTO-THROTTLE TESTS REF B767 AMM 22-33-01 + 22-00-02. ALL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 94,335 hrs · 34,901 cycles

CENTER FUEL QTY BLANK WITH TOTALIZER DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED CENTER TANK FUEL QUANTITY INDICATION IAW MEL 28-41-1-2. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — CRACKED (LOWER TAIL SECTI) · airframe 93,843 hrs · 34,775 cycles

AFTER TAKEOFF DURING GEAR/FLAP RETRACTION LOSS OF ALL CENTER HYD FLUID AND PRESSURE. USED ALT FLAP AND GEAR EXTENSION AND RETURNED TO CVG FOR A HEAVY WEIGHT (362,000 #) LANDING. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND TAIL SKID CONTROL MODULE DAMAGED AND WAS THE SOURCE FOR THE HYDRAULIC FLUID LOSS. MAINTENANCE REMOVED AND REPLACED TAIL SKID CONTROL MODULE IAW B767 AMM 32-71-01. SERVICED CTR HYD IAW B767 AMM 12-12-01. PERFORMED OVERWEIGHT LANDING INSPECTION IAW B767 AMM 05-51-35. CONDUCTED HIGH ENERGY STOP INSPECTION PER AMM 05-51-14 PARA 2. B. NO FUSE PLUGS DISCHARGED. AFTER 3 HOURS, BRAKES COOLED, NO CAUTION ON BRAKE TEMP. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAULTED (LEFT ENGINE) · airframe 93,453 hrs · 34,661 cycles

DURING TAXI LEFT ENG BLEED EICAS MESSAGE, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED & REPLACED LH ENG PRSOV IAW B767 AMM 36-11-09. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (ZONE 100) · airframe 93,263 hrs · 34,599 cycles

PARKING BRAKE EICAS MESSAGE WHEN PARKING BRAKE LEVER RELEASED. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDEDD BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE PARKING BRAKE VALVE 32-44-04 OPS NORMAL. PART EFFECTIVITY VERIFIED. AIRCRAFT RETURNED TO SERVICE.

Part: SPRING — BROKEN (COCKPIT) · airframe 92,934 hrs · 34,517 cycles

DURING TAKE-OFF ROLL, CAPT’S SEAT ROLLED BACK. ABORTED TAKE-OFF. AS A SIDE NOTE , BRAKE TEMPS WENT TO 7 AND 8’S DUE TO THE ABORTED TAKE-OFF.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED BROKEN SPRING ON HORIZONTAL ADJUSTMENT LEVER. OPS CHECKS NORMAL IAW B767 AMM 25-11-01. COMPLIED WITH HIGH ENERGY STOP INSP. IAW B767 AMM 05-51-14. FOUND #6 MAIN TIRE PARTIALLY DEFLATED. NO OTHER DAMAGE NOTED. REMOVED AND REPLACED #5 & #6 MAIN TIRE/WHEEL ASSYS. IAW B767AMM 32-45-01. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 92,884 hrs · 34,504 cycles

AUTOTHROTTLE DISC LIGHT CAME ON DURING PUSHBACK RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE CONDUCTED TEST 02 AND 10, NO FAULTS FOUND. REF AMM 22-00-02. A/C RELEASED PENDING TEST 30/40 TO CAT I PLACARD ROTATED.CONDUCTED TEST 30/40 PER AMM 22-00-02. NO FAULTS AT THIS TIME. A/C RELEASED CAT IIIB PLACARD ROTATED.AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTED (TE FLAPS) · airframe 90,158 hrs · 33,590 cycles

ABORTED T/O FOR RED FLAPS EICAS MESSAGE WITH FLAPS IN THE "5" POSITION, ALSO GOT A "NO LAND 3" FLAG. AIRCRAFT BACK TO GATE, GROUNDED BY MAINTENANCE. BITE CHECK OF PSEU, FSEU AND FSPM'S, SHOW CENTER FSPM WITH MODULE FAULT. REMOVED AND REPLACED CENTER FSPM, IAW B767 AMM 27-61-00. BITE CHECK GOOD FOR TAKE OF CONFIG BITE CHECK GOOD. A/C DOWNGRAFED TO CAT I PENDING 30/40 CHECKS, AICRAFT RELEASED.

Part: MODULE — INTERMITTENT (STAB TRIM) · airframe 90,032 hrs · 33,548 cycles

STAB TRIM EICAS MESSAGE DURING CLIMB OUT OF PTY. FLIGHT WAS SCHEDULED TO SJU, FLIGHT CREW ELECTED TO DIVERT TO MIA. AIRCRAFT WAS GROUNDED IN MIA. MAINTENANCE COMPLIED WITH FIM 27-09 F/T 811 SAM BIT PROCEDURE, PASSED. COMPLIED WITH FIM 27-48 F/T 809, NO STCM FAULTS ON THE LEFT OR RIGHT SAM, PERFORMED STAB TRIM COLUMN CDT-00 TEST IAW AMM 27-11-00, OPS NORMAL. RANG WIRING BETWEEN THE LEFT SAM AND LEFT STCM NO DEFECTS. RIGHT SAM AND RIGHT STCM NO DEFECTS PER WDM 27-41-11 AND 27-41-21. MCDP FAULTS SHOWED LEFT STCM FAULTING 2 TIMES. RECOMMENDED REPLACEMENT DUE TO THE INTERMITTENT NATURE. REPLACED LT STABILIZER TRIM CONTROL MODULE, IAW AMM 27-41-05.

Part: MODULE — FAULTED (STAB TRIM) · airframe 89,659 hrs · 33,423 cycles

UNSCHEDULED STAB TRIM EICAS MEESAGE AND AURAL WARNING DURING TAKE-OFF ROLL, ABORTED TAKEOFF AT 85 KNOTS.AIRCRAFT WAS GROUNDED. TROUBLESHOT USING FIM 27-09 FT 813, FOUND STCM FAULT BALL ON THE LEFT SAM, FAULT BALL CLEARED AND SYSTEM TEST NORMAL REMOVED AND REPLACED THE LEFT SAM IAW 27-09-00 AND 27-11-00, TEST OK

Part: WARNING MESSAGE — ILLUMINATED (STAB TRIM) · airframe 89,527 hrs · 33,376 cycles

UNSCHEDULED STAB TRIM EICAS AND MASTER WARNING ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF AT 60 KNOTS. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 89,524 hrs · 33,373 cycles

CRACK AT MAIN CABIN FLOOR BETWEEN STUB FITTING AND FLOOR BEAM. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (L1 DOOR) · airframe 89,524 hrs · 33,373 cycles

CRACK L1 DOOR AT AFT LOWER INNER RADIUS. AIRCRAFT WAS GROUNDED.

Part: BEAM — CORRODED (LT WING TE FLAP) · airframe 89,524 hrs · 33,373 cycles

GOUGE ON LH WING INBD FLAP OUTBD FLAP TRACK AFT FITTING INBD SIDE. AIRCRAFT WAS GROUNDED.

Part: STIFFENER — CORRODED (LT WING SLAT) · airframe 89,524 hrs · 33,373 cycles

LH WING SLAT NR 2 INBD PANEL MOUNT FLANGE HAD CORROSION AT OTBD UPPER CORNER; REPLACED. AIRCRAFT WAS GROUNDED.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 89,496 hrs · 33,361 cycles

AFT CABIN TEMPERATURE EICAS MESSAGE. AIRCRAFT WAS GROUNDED.

Part: CONTROL UNIT — FAULTY (HYDRAULIC SYS) · airframe 89,040 hrs · 33,149 cycles

L HYD QTY EICAS + LHYD SYS PRESS EICAS + RUDDER RATIO EICAS + RT YAW DAMPER EICAS MESSAGES DISPLAYED. HYDRAULIC CONTROL UNIT WAS REPLACED. AIRCRAFT WAS GROUNDED. MAINTENANCE SUSPECTS FAULTY VALVE FOR EICAS MESSAGES.

Part: WIRE — DAMAGED (CARGO DOOR) · airframe 88,748 hrs · 33,023 cycles

THE AFT LOWER CARGO DOOR WOULD NOT CLOSE ELECTRICALLY. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE AFT LOWER CARGO DOOR ELECTRICAL SYSTEM'S WIRING WAS INSPECTED. IN THE FORWARD LOWER CARGO COMPARTMENT, DAMAGED WIRES WERE FOUND BEHIND A WALL PANEL. SOME WIRES APPEARED BURNT. THE WIRES WERE REPAIRED. THE SUSPECTED CAUSE OF THE DAMAGED WIRES WAS INADEQUATE CLEARANCE BETWEEN THE WALL PANEL FASTENER AND THE WIRE BUNDLE.

Part: GUARD — OUT OF POSITION (EMEGENCY LT SWCH) · airframe 88,342 hrs · 32,853 cycles

THE EMERGENCY LIGHT SWITCH DISARMS WHEN THE GUARD IS CLOSED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE EMERGENCY LIGHTS CAPTURE MECHANISM IN THE SWITCH GUARD WAS REPOSITIONED.

Part: PANEL — MISSING (RT PYLON) · airframe 87,506 hrs · 32,471 cycles

RIGHT ENGINE PYLON AFT OUTBOARD SIDE PANEL ASSEMBLY IS MISSING PANEL NUMBER 446AL. THE PANEL POSSIBLY DEPARTED DURING OPERATION OF THE AIRCRAFT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND A SERVICEABLE PANEL 446AL WAS INSTALLED. THE CAUSE OF THE MISSING PANEL IS UNKNOWN.

Part: MANIFOLD — SEPARATED (LT ENGINE) · airframe 87,304 hrs · 32,379 cycles

THE LEFT ENGINE 14TH STAGE MANIFOLD ASSEMBLY SEPARATED OUTBOARD OF THE COUPLING AT ONE OF THE ENGINE'S THREE HIGH PRESSURE BLEED PORTS. THIS CAUSED A LEFT ENGINE FIRE INDICATION WITH THE OVERHEAT LIGHT ILLUMINATED IN THE FLIGHT DECK DURING CLIMB AFTER TAKEOFF. THE CREW PERFORMED AN IN-FLIGHT SHUT DOWN OF THE LEFT ENGINE, DECLARED AN EMERGENCY, AND RETURNED TO THE AIRPORT (CVG). THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE'S 14TH STAGE MANIFOLD ASSEMBLY WAS REPLACED. ALSO REPLACED AT THE LEFT ENGINE WERE THE BONDING STRAP FOR THE PRESSURE REGULATING VALVE, THE ENGINE FIRE AND OVERHEAT DETECTION WIRING, AND THE COOLING HOSE FOR THE THROTTLE PUSH-PULL CABLE COOLING SYSTEM. THE STRAP, WIRING, AND THE HOSE WERE DAMAGED BY THE PNEUMATIC AIR ESCAPING FROM THE FAILED 14TH STAGE MANIFOLD ASSEMBLY. THE CAUSE OF THE 14TH STAGE MANIFOLD ASSEMBLY FAILURE IS UNKNOWN. ENGINE FIRE INDICATION ON THE FLIGHT DECK BUT THERE WAS NO ENGINE FIRE.

Part: BLOWER — FAULTY (CARGO BAY) · airframe 86,758 hrs · 32,145 cycles

"FWD CARGO FIRE" EICAS MESSAGE REPORTED BY THE FLIGHT CREW TO DISPLAY DURING FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE FORWARD LOWER CARGO COMPARTMENT WAS INSPECTED. THERE WAS NO SIGNS OF FIRE. THE FORWARD CARGO SMOKE DETECTOR AIR FLOW BLOWER 2 ((M717) BODY STATION 352, WATER LINE 164, LEFT BUTT LINE 70) WAS FOUND HOT WITH A BURNT ODOR. THE AIR FLOW BLOWER WAS REPLACED. THE SUSPECTED CAUSE OF THE "FWD CARGO FIRE" EICAS MESSAGE WAS THE FAULTY FORWARD CARGO SMOKE DETECTOR AIR FLOW BLOWER 2.

Part: DRIVE SHAFT — DISCONNECTED (TE FLAP) · airframe 86,482 hrs · 32,028 cycles

AFTER TAKEOFF, THE “TE FLAP ASYM” EICAS MESSAGE ILLUMINATED. THE LEFT FLAP INDICATOR SHOWED APPROXIMATELY 4 DEGREES OF FLAPS, AND THE RIGHT FLAP INDICATOR SHOWED 5 DEGREES. MOVING THE FLAP LEVER HAD NO EFFECT ON THE FLAPS. THE CREW PERFORMED AN AIR TURN BACK AND LANDED WITH FLAPS IN FROZEN POSITION. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE FLAP DRIVE SHAFT WAS FOUND DISCONNECTED FROM THE RIGHT AILERON DROOP ANGLE GEARBOX ASSEMBLY AT RIGHT WING STATION 452. THE THREE DRIVE SHAFT TO GEARBOX CONNECT BOLTS WERE FOUND IN THE TRAILING EDGE WING WELL. THE CAUSE OF THE DRIVE SHAFT DISCONNECTION IS UNKNOWN.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 85,605 hrs · 31,661 cycles

CORROSION ON THE LEFT WING REAR SPAR TO TRAILING EDGE, UPPER PANEL ATTACH BEAM AT LWS 285. THE ATTACH BEAM AND UPPER PANEL WERE REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — GOUGED (BS 618) · airframe 85,605 hrs · 31,661 cycles

GOUGE FOUND ON THE SKIN, AT THE AFT EDGE OF THE FORWARD LOWER CARGO DOOR AT BS 618. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,605 hrs · 31,661 cycles

CORROSION FOUND ON THE RIGHT WING LOWER SKIN PANEL NR 1, RWS 918. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.

Part: SKIN — DAMAGED (BS 654) · airframe 85,605 hrs · 31,661 cycles

EXTERNAL SKIN HAD TWO FASTENER HOLES, AT THE EDGE OF SKIN AT BS 654+22 WAS DAMAGED AT STRINGER 16L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 85,605 hrs · 31,661 cycles

CORROSION ON THE RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH BEAM AT WING STATION 280. THE UPPER PART OF THE ATTACH BEAM WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · airframe 85,605 hrs · 31,661 cycles

CORROSION FOUND ON THE RIGHT WING, LOWER SKIN, RWS 924.16. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.

Part: BEAM — GOUGED (LT WING TE FLAP) · airframe 85,605 hrs · 31,661 cycles

GOUGES ON THE INBOARD FLAP INBOARD TRAILING EDGE BEAM AT WING STATION 344.3. THE BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: UNKNOWN — MALFUNCTIONED (THRUST LEVER) · airframe 81,860 hrs · 30,350 cycles

AFTER LANDING, THE LEFT THRUST LEVER WOULD NOT MOVE FROM IDLE FOR ONE MINUTE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE ADJUSTMENT TEST PROCEDURE WAS PERFORMED IN ACCORDANCE WITH AMM 78-31-00. NO FAULTS WERE FOUND. THE CAUSE OF THE FAULT WITH THE LEFT THRUST LEVER WAS NOT DETERMINED.

Part: ANGLE — CORRODED (248-375) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

CORROSION INTERIOR OF THE AFT 437BR ACCESS AFT UPPER CORNER, NEAR THE AFT HINGE OF THE LEFT ENGINE NAC STRUT AFT FAIRING. CORROSION WAS BLENDED OUT OF LIMITS, REPLACED THE UPPER ANGLE IN THE HYDRAULIC BAY IN ACCORDANCE WITH SRM 51-40-02 SECTION 7. AIRCRAFT GROUNDED.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

LEFT WING LEADING EDGE LOWER CHORD SPLIT ON EDGE WHERE NUMBER 5 SLAT INBOARD DRIVE ROD DOOR CONTACTS. REMOVED DAMAGE SPLICE PLATE AT LEFT WING STATION 330.475. INSTALLED NEW SECTION OF SPLICE PLATE IN ACCORDANCE WITH 472222REA01 AND SRM 51-40-02. AIRCRAFT GROUNDED.

Part: ATTACH ANGLE — CRACKED (THRUST REVERSER) · airframe 81,395 hrs · 30,124 cycles

ACFT GROUNDED FOR HEAVY MAINTENANCE. INBD THRUST REVERSER ATTACH ANGLES FORWARD OF CASCADE VANES CRACKED AT 1:00 POSITIONS AS SEEN WITH SLEEVE DEPLOYED. R & R INBD ATTACH ANGLES IAW SRM 51-41-01.

Part: STIFFENER — CRACKED (THRUST REVERSER) · airframe 81,395 hrs · 30,124 cycles

INBOARD THRUST REVERSER ATTACH ANGLE FORWARD OF CASCADE VANES CRACKED AT 4:00 POSITION AS SEEN WITH SLEEVE DEPLOYED. REMOVED AND REPLACED INBOARD ATTACH ANGLES IAW SRM 51-41-01.

Part: SPLICE — CORRODED (LT WING) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

CORROSION ON LEFT WING LEADING EDGE LOWER CHORD AT FUELING PANEL ADJACENT TO DOOR INBOARD LATCH PLATE. BLENDED CORROSION OUT OF LIMITS AND REPLACED LOWER CHORD SPLICE STRAP IN ACCORDANCE WITH B767 SRM 51-40-02 SECTION 7.

Part: ATTACH FITTING — CORRODED (MLG) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

ATTACH FITTING ON LOWER LANDING GEAR AUXILIARY BEAM EXFOILIATED. LOCATED ABOVE LOWER LANDING GEAR STRUT DOOR AFT END. BLENDED OUT OF LIMITS, REMOVED AND REPLACED THE ATTACH FITTING ON LOWER LANDING GEAR AUXILIARY BEAM IAW SRM 51-40-02 PART 7. ACFT GROUNDED.

Part: SKIN — CRACKED (BS 1654) · airframe 81,395 hrs · 30,124 cycles

LEFT FUSELAGE SKIN CRACKED BS 1654 BETWEEN STRINGERS 4 - 6R. REPAIRED THE SKIN IAW SRM 53-80-01 REPAIR 4.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

RIGHT WING UPPER SURFACE AT WS 273 STRINGER 17R CORRODED. BLENDED OUT CORROSION IAW SRM 57-20-01. REPAIRED BLEND OUT IAW DRAWING 57-16116-1.

Part: SKIN — CRACKED (BS 1723) · airframe 81,395 hrs · 30,124 cycles

INDICATIONS OF CRACK ON OUTSIDE OF SKIN COMING FROM 2 FASTENER HOLES AT APPROXIMATELY BS 1723. REPAIRED THE SKIN IAW 53-00-01 FIGURE 201. ACFT GROUND.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 81,395 hrs · 30,124 cycles

UPPER FWD CORNER OF BULK CARGO DOOR HAS CORROSION AT HINGE LOWER MOUNT BOLTS ON INNER SKIN. BLENDED AREA OUT OF LIMITS. REPAIRED BULK CARGO DOOR IN ACCORDANCE WITH B767 SRM 51-70-13 FIGURE 1. AIRCRAFT GROUNDED.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 79,605 hrs · 29,377 cycles

EMERGENCY DOORS DISCREET LIGHT ON OVERHEAD PANEL ILLUMINATES INTERMITTENTLY, NO ACCOMPANYING EICAS MSG. R & R EMER DOORS DISCRETE LIGHT ASSEMBLY ON OVERHEAD PANEL IAW WPSM 20-84-18. OPERATIONAL CHECKED SATISFACTORY.

Part: COMPUTER — FAILED (AUTOPILOT) · airframe 77,634 hrs · 28,575 cycles

ENROUTE, LEVEL AT FL350 CENTER AUTOPILOT SHORTLY THERE AFTER NOTED BRIEF ODOR OF SMOKE. DEFERRED, CLEARED 10/08/2013-PERFORMED OHM CHECK OF WIRING FROM FCC COMPUTER TO AILERON, DIRECTIONAL AND ELEVATOR SERVO'S NO DEFECTS NOTED. R & R CENTER FCC IAW AMM 22-11-01. PLACARD REMOVED. PN VERIFIED. ACFT RELEASED TO CAT II, CHECK CAT IIIB.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 77,630 hrs · 28,572 cycles

LEFT HORIZONTAL STABILIZER HAS A SPOT OF CORRORSION ON UPPER SURFACE AT HSBL 264. BLENDED AREA OF CORROSION ON UPPER SURFACE AT HSBL 24 IAW SRM 51-10- 00. REPAIRED SKIN BLENDOUT IAW REA B655-60721-MR. CLOSED ACCESS PANELS IAW SRM 51-40-02, PAR 7. LEVEL 2 CORROSION, PN: 182T3200-1, SKIN, RS STA 251 TO RS STA 251 L/E. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 77,630 hrs · 28,572 cycles

LEFT HORIZONTAL STAB HAS A SPOT OF CORROSION ON UPPER SURFACE AT HSBL 336. REPAIRED DAMAGE CAUSE BY CORROSION IAW REA B655-60720-MR. LEVEL 2 CORROSION, PN: 182T3200, SKIN PANEL, HSRL 334 TO HSBL 336, REAR SPAR TO REAR SPAR. ACFT WAS GROUNDED.

Part: ACCESS PANEL — CORRODED (ZONE 100) · airframe 77,630 hrs · 28,572 cycles

FOUND CORRORSION ON AFT FLANGE FOR REFUELING PANEL 521QB. REMOVED CORROSION IAW SRM 51-10-02 COMPLIED WITH REA 657-60710. ACFT WAS GROUNDED.