N708AX

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,975 hrs · 20,131 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOP. DEFERRED NR 62289, SWAPPED EMERGENCY BATTERY PACKS P/N 2013-1A, S/N 60781 AND LOWER S/N 61030 AS REQUIRED. OPS CHECK NORMAL. DEFERRED FOR TRACKING IAW 767 GMM 07.04 PLACARD INSTALLED CODE 11. CLEARING DI 62289. REMOVED AND REPLACED LOWER EMERGENCY LIGHTING BATTERY PACK. OPS CHECKS GOOD IAW B767 AMM 33-51-00. PLACARD REMOVED. NOTE: PART REMOVED WAS 'F' CLASS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,252 hrs · 19,800 cycles

ON PRE-DEPARTURE CHECK AT STA SAN, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED WITH SPARE BATTERY PACK IAW B767 MM 33-51-07-02.

Part: BULB — MALFUNCTIONED (OIL TEMP) · airframe 77,040 hrs · 19,689 cycles

708AX MADE A DIVERSION TO STA - PHX, NR 2 ENGINE SHUT DOWN DURING CRUISE DUE TO HIGH OIL TEMP, HIGHEST NOTED TEMP 173 DEGREES. ALL OTHER INDICATION APPEARED NORMAL. REPLACED RIGHT ENGINE OIL TEMP BULB IAW ABX B767 MM 79-34-00-4. TEMP SEPERATION REMAINED CONSTANT THROUGHOUT RISE. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (MLG INDICATOR) · airframe 76,395 hrs · 19,390 cycles

ABORTED APPROACH AT MHR. NOSE GEAR FAILED TO ILLUMINATE ON GEAR SELECT DOWN, NO LIGHT IN GEAR INDICATION LIGHT TEST. DID ALT GEAR EXTEND PROCEDURE AND HAD TOWER CONFIRM NOSE GEAR DOWN. VERIFIED NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE ON LIGHTS TEST. REPLACED BOTH BULBS IAW ABX 767 AMM 33-16-02, OPS CHECKED GOOD. NOSE GEAR WAS DOWN AND LOCKED AND INDICATION AGREED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,856 hrs · 19,189 cycles

ON PRE-DEPARTURE CHECK, FOUND WHEN EMERGENCY LIGHT SWITCH SELECTED TO ON, LIGHTS ILLUMINATED MOMENTARILY, THEN EXTINGUISHED. SWAPPED SPARE AND ACTIVE EMERGENCY POWER SUPPLIES. OPS CHECKED GOOD IAW B767 MM 33-51-07-2.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 75,681 hrs · 19,122 cycles

ON TAKEOFF FROM ILN, DURING LANDING GEAR RETRACTION, GOT SUBSTANTIAL IMPACT SOUND FROM LEFT ENGINE AREA, AND BURNING SMELL AFTER SOUND. NO ENGINE ABNORMALITIES OR EXCEEDANCES. LANDED UNDER WEIGHT. C/W BIRD STRIKE INSPECTION BORESCOPE & BLADE REPLACEMENT ON LT ENGINE REF W/P 600264766 FOR DOCUMENTATION. MAINTENANCE PULLED THE THREE DAMAGED BEYOND LIMIT BLADES AND ADDITIONAL 180 BLADE FOR A TOTAL OF FOUR BLADES THAT NEED CHANGED. AIRCRAFT TOOK SOME BIRDS AS WELL, BUT NO DENTS ON AIRFRAME FOUND.

Part: PRESSURE SWITCH — DEFECTIVE (RT ENGINE) · airframe 72,811 hrs · 18,023 cycles

IN FLIGHT, RIGHT OIL FILTER LIGHT DID NOT GO OUT WITH TRUST REDUCTION. RT ENGINE WAS SHUT DOWN. WINDMILLED FOR 31 MINUTES, OIL PRESSURE UNKNOWN. FOUND THE RIGHT OIL FILTER DIFFERENTIAL PRESSURE SWITCH DEFECTIVE. REPLACED THE SWITCH. COMPLIED WITH NR 2 ENGINE WINDMILL AND BOROSCOPE INSPECTION. NO DEFECTS WERE FOUND.

Part: A/C PACK — SHUTDOWN (AIR CONDITIONING) · airframe 70,848 hrs · 17,335 cycles

DURING APPROACH TO RUNWAY 22L AT MHR, WHEN LANDING GEAR WAS LOWERED, RIGHT PACK SHUT OFF AND LOC FAILED. MISSED APPROACH EXECUTED, GEAR CYCLED UP AND DOWN AND EVERYTHING SEEMED TO WORK AGAIN. MAINTENANCE AT MHR COMPLIED WITH MCDP GROUND TEST 30. NO CURRENT FAULTS NOTED. A/C RELEASED TO CAT 2 CHECK CAT 3B.

Part: ACOUSTIC LINER — MISSING (NR 2 ENGINE) · airframe 70,070 hrs · 17,071 cycles

NR 2 ENGINE REVERSER OUTBOARD SIDE INNER AREA HAD DAMAGE DUE TO LIBERATION OF A P/N 803723 ENGINE FAN EXIT CASE OUTBOARD ACOUSTIC LINER SEGMENT ASSEMBLY, WHICH RAN FROM THE 3 O'CLOCK TO THE 5 O'CLOCK POSITION, AFT FACING FORWARD. REPLACED NR 2 ENGINE OUTBOARD REVERSER IAW BMM 767 78-31-01-4. OPS CHECKED GOOD.

Part: ACTUATOR — DEFECTIVE (SPOILER) · airframe 69,075 hrs · 16,713 cycles

SPOILERS LIGHT ILLUMINATED EICAS MESSAGE SPOILERS DISPLAYED WITH SPOILERS SELECTED DOWN. THIS HAPPENED IMMEDIATELY AFTER TAKEOFF. AT FL 350, CONTROL WHEEL DISPLAYED AN UNCOMMANDED 45 DEGREES WITH AUTOPILOT ENGAGED. AUTOPILOT WAS DISCONNECTED AND THE UNCOMMANDED CONTROL DISPLACEMENT REMAINED AT FLIGHT LEVEL 240. ALL CONTROL INPUTS APPEARED NORMAL. FOUND CONNECTOR D161 SLIGHTLY BURNED. REMOVED AND REPLACED CONNECTOR D161 AND THREE SOCKETS IAW B767 WDM 27-61-13. REMOVED AND REPLACED SPOILER ACTUATOR NR 12 IAW B767 MM 27-61-02-4.

Part: DOOR FRAME — CONTAMINATED (MAIN PAX DOOR) · airframe 68,675 hrs · 16,573 cycles

EMERGENCY SLIDE WOULD NOT ARM. FOUND DEBRIS IN MAIN ENTRY DOOR JAMB, REMOVED DEBRIS. DOOR CLOSED AND EMERGENCY SLIDE ARMED AS REQUIRED IAW B767 MM.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR) · airframe 67,584 hrs · 16,189 cycles

THE FORCE TO MOVE THE MAIN ENTRY DOOR TO THE CLOSED POSITION WAS EXCESSIVE. COMPLIED WITH ENTRY DOOR COUNTERBALANCE ADJUSTMENT IAW 767 AMM 52-11-16. OPS CHECKED GOOD.

Part: MODULE — FAULTY (COCKPIT) · airframe 64,914 hrs · 15,305 cycles

EICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GEAR. GREEN DOWN LIGHT ILLUMINATED. ALSO EICAS MESSAGE LANDING MONITOR DISPLAYED WITH LANDING GEAR UP AND LOCKED. DID GEAR RECYCLE AND OVERFLEW STATION. REPLACED LANDING GEAR CONTROL LEVER MODULE ASSEMBLY IAW B767 MM 32-31-01-04. PERFORMED BITE CHECK ON PSEU. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (LT ENGINE) · airframe 66,297 hrs · 15,753 cycles

FRM CODE FOR LEFT ENGINE VIBRATION HIGH INDICATED. OTHER ENGINE INDICATIONS WERE NORMAL. VIBRATION INDICATION CHANGED WITH THRUST LEVER MOVEMENT. HIGHEST INDICATION WAS 1.5 IPS. FAN /LPT0.6 IPS N2. MAINTENANCE COMPLETED ABX767 FIM 71A 05.00 PROCEDURES. CLEANED MINOR OXIDATION FROM LEFT ENGINE FAN VIBRATION ACCELEROMETER CONNECTOR. COMPLETED LEFT ENGINE RUN. THE ENGINE VIBRATION SYSTEM OPERATIONALLY CHECKED GOOD.