N786AX

Part: HEAT SHIELD — CRACKED (RT PYLON) · airframe 52,973 hrs · 40,703 cycles

RIGHT WING HEAT SHIELD BRACKET ABOVE EXHAUST CONS AND AFT OF ENGINE (AFT) MOUNT CRACKED ON PYLON STRUT. REMOVED DAMAGED HEAT SHIELD BRACKET AND REPAIRED IAW AMES PROCESS STANDARDS MANUAL CH 7 SEC 3 DATED 3/2/12 REV 12. RE-INSTALLED BRACKET IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 52,973 hrs · 40,703 cycles

LOWER LEFT WING AT OUTBOARD END AFT OF OUTBOARD LOWER ACCESS PANEL HAS AREA OF SUSPECT CORROSION: SKIN BULGING WS 1106. REMOVED AND REPLACED LOWER WING PANEL, ACFT WAS GROUNDED.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 52,973 hrs · 40,703 cycles

EXISTING REPAIR AT STA 1725.5 AT STR 7R IS NOT IAW SRM 53-80-01-2R-5, REPAIR 5, DETAIL II. FASTENER PATTERN & TYPE IS DIFFERENT FROM DETAIL II BY HAVING HI-LOKS IN PLACE OF SOME BACR15CE6KE RIVETS. PRESENCE OF TRIPLER IS OBSCURED BY PAINT & NOT VISUALLY VERIFIABLE. REMOVED AND REPLACED REPAIR AT STA 1725.5 L7R IAW B767 SRM 53-80-01 2R5 FIG 201 REPAIR 5 DETAIL II, ACFT WAS GROUNDED.

Part: MOUNT — CORRODED (NHR 1 ENGINE) · airframe 52,973 hrs · 40,703 cycles

NR 1 ENGINE AFT MOUNT CORRODED AT THE INBOARD LWR PORTION AND THE OUTBOARD FWD AREA. REMOVED AND REPLACED AFT ENGINE MOUNT AS REQUIRED IAW B767 AMM CONFIG 10 71-21-02-4, ACFT WAS GROUNDED.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 51,043 hrs · 39,574 cycles

LAVATORY SMOKE ALARM SOUNDED DURING FLIGHT - NO SMOKE. REMOVED AND REPLACED SMOKE ALARM IAW 26-13-01-4. NO DEFECTS NOTED.

Part: STRUCTURE — CHAFED (NACELLE) · airframe 51,041 hrs · 39,572 cycles

AREA ON INBOARD ENG STRUT BOX CHAFED WHERE UPPER AFT PART OF T/R MEETS STRUT BOX FWD OF CORE COWL. CHAFE AREA BLENDED BEYOND LIMITS B767 SRM 54-51-01. REQUIRED REPAIR. REPAIRED DAMAGE IAW REA B654-59113-MR.

Part: SKIN — CHAFED (NR 2 NACELLE) · airframe 51,041 hrs · 39,572 cycles

NR 2 STRUT RT SIDE, THE SURFACE OF THE STRUT IS CHAFED (6 INCHES LONG) AND DENTED JUST BELOW AN ANGLE WHERE THE UPPER SECTION OF THE REVERSERS AFT LOWER CORNER MEETS THE STRUT. REPAIRED CHAFED AND DENTED AREA IAW REA B654-59111-MR.

Part: INTERCOSTAL — CORRODED (RT WING) · airframe 51,041 hrs · 39,572 cycles

RT WING L/E INTERCOSTAL LEG CORRODED AT WS 860 UNDER PANEL 621ZB. REMOVED AND REPLACED NOSE BEAM IAW BOEING DWG 114T2300 & B767 SRM 51-40-02.

Part: RIB — CORRODED (CARGO DOOR) · airframe 51,041 hrs · 39,572 cycles

RIB IN FLC DOOR BELOW RELIEF DOORS AND VERTICAL STRAP BELOW FWD END OF SAME RIB CORRODED AROUND NUT PLATE HOLES. REMOVED AND REPLACED DAMAGED T-ANGLE IAW B767-200 SRM 51-40-02.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 51,025 hrs · 39,568 cycles

DURING CARGO MODIFICATION AT IAI DISCOVERED WING CENTER SECTION FRONT SPAR STIFFENER CRACKED. REPAIRED IAW REA B657-58877MR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,830 hrs · 39,482 cycles

EMERGENCY LIGHTS INOP. DEFERRED DI 62414 SPARE EMERGENCY LIGHT BATTERY DEFERRED FOR MAINT TRACKING IAW ABX GMM 01.07.04 REPLACE WITHIN 7 DAYS DEFERRED PER B767 AMM 33-51-07-2 PLACARD INSTALLED MBCB 11-22-08. CLEAR DI 62414 REMOVED BOTH BATTERYS, CHECK BOTH BATTERY CHARGER, BOTH OPERATE NORMALLY, REINSTALLED PRIMARY BATTERYS, INSTALLED NEW BATTERY IN SECONDARY POSITION, CHECK SYSTEM PER 33-51-07-2, OPS CKS NORMALLY.

Part: EEC — DEFECTIVE (LT ENGINE) · airframe 50,215 hrs · 39,260 cycles

CLOSE TO V1 SPEED, LT EEC LIGHT, THEN LT ENG OVERTEMP LIGHT. ENG WENT TO 974, WHEN THRUST LEVEL RETARDED, LIGHT OUT. REMOVED AND REPLACED LT ENG EEC IAW B767 MM 73-21-07-04. EEC TEST GOOD, OPS CHECK GOOD ON GROUND RUN IAW 767 AMM 72-00-00-0. (S)

Part: PUMP — DEFECTIVE (HYD SYSTEM) · airframe 49,738 hrs · 39,126 cycles

EDP HYDRAULIC PRESSURE LOW - LOW PRESSURE LIGHT ILLUMINATED. HAD EICAS MESSAGE LEFT HYDRAULIC PRIMARY PUMP. REMOVED AND REPLACED NR 1 ENG DRIVEN HYDRAULIC PUMP IAW B767 MM 29-11-05-4. OPS CHECKED GOOD. (S)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,587 hrs · 39,056 cycles

ALL EMERGENCY LAMPS INOPERATIVE. DEFERRED: 59239. EMERGENCY LIGHT BATTERY PACKS SWAPPED FROM PRIMARY TO SPARE POSITIONS. OPS CHECKED GOOD. ALL WORK DONE IAW AMM 33-51-07-2. THE SPARE EMERGENCY LIGHT BATTERY HAS BEEN DEFERRED FOR TRACKING IAW ABX GMM 01-07-04. CLEARED DI: REMOVED AND REPLACED THE SPARE EMERGENCY LIGHTS BATTERY PACK IAW B767 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,599 hrs · 38,713 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. SWITCHED BATTERY PACKS IAW B767 MM 33-52-07. OPS CHECKED GOOD. USED SPARE EMERGENCY EXIT LIGHT BATTERY PACK. PART IS -F- CLASS, NOT RELIABILITY PART.

Part: FUEL CONTROL — DEFECTIVE (RIGHT ENGINE) · airframe 45,430 hrs · 37,551 cycles

ON TAKEOFF ROLL, RIGHT ENGINE FAILED TO PRODUCE TAKEOFF POWER. WITH LEFT ENGINE ACCELERATING NORMALLY. RIGHT ENGINE STOPPED ACCELERATING AT 58 PERCENT N1. REMOVED AND REPLACED RIGHT ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-4. PERFORMED ENGINE RUN, SYSTEM CHECKED GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (MLG) · airframe 42,562 hrs · 36,531 cycles

INFLT, COMPLETING AFTER TAKEOFF CHECKLIST, UPON MOVING GEAR LEVER TO OFF, EICAS MESSAGE GEAR DOOR AND AMBER DOOR LIGHT ILLUMINATED. PUSHED LOCK OVERRIDE AND RETURNED HANDLE TO UP POSITION. LIGHTS EXTINGUISHED. GEAR WAS CYCLED. COULD NOT VERIFY. INSPECTED MAIN AND NOSE GEAR DOORS FOR SECURITY. CHECKED PSEU FOR PROXIMITY SENSOR FAULTS AND TARGET TESTED, NEAR-FAR, BOTH MAINS AND NOSE PER AMM 32-09-04-4. NO FAULT FOUND. CHECKED LANDING GEAR POSITION INDICATION AND WARNING SYSTEM PER 32-61-00-5-11. CHECKED GOOD.

Part: FAN — VIBRATION (RT ENGINE) · airframe 42,047 hrs · 36,360 cycles

RT ENGINE FAN VIBRATION INDICATIONS WERE HIGH. BETWEEN 2.5 AND 3.5, FL 390, M .80. ACCOMPANIED BY AIRFRAME/ENGINE VIBRATION. SETTLED BACK TO 1.5 THEN BACK TO 3.0. THIS CONTINUED FOR APPROXIMATELY 30 MINUTES THEN WENT AWAY. PERFORMED FIM 71-05-00-60, NO DEFECTS NOTED. PERFORMED AMM 71-00-00-5, TEST NR 7, ENGINE VIBRATION WITHIN LIMITS. ENGINE WITHIN LIMITS IAW AMM 71-00-00-2, PARA. J.

Part: TUBE — WORN (LEFT LCCA) · airframe 39,931 hrs · 35,624 cycles

LEFT LCCA CONTROL TUBE ASSEMBLY HAD WORN PIVOT BEARINGS. REPLACED LEFT LCCA TRUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD.

Part: TUBE — WORN (RT LCCA) · airframe 39,931 hrs · 35,624 cycles

RIGHT LCCA TUBE ASSEMBLY HAD WORN/RUSTED PIVOT BEARINGS. REPLACED LCCA TUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD.

Part: BEARING — WORN (LT ELEVATOR) · airframe 39,931 hrs · 35,624 cycles

LEFT ELEVATOR, OUTBOARD PCA HAD A WORN AFT ATTACH BEARING. REPLACED ELEVATOR PCA IAW B767 MM. OPS CHECKED GOOD.

Part: BEARING — WORN (RT AILERON) · airframe 39,931 hrs · 35,624 cycles

RT OUTBOARD AILERON, OUTBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD.

Part: BEARING — WORN (RT AILERON) · airframe 39,931 hrs · 35,624 cycles

RT OUTBOARD AILERON, INBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD.

Part: ENGINE — VIBRATION (ENGINE) · airframe 38,265 hrs · 35,061 cycles

CLIMB READING WAS 2.7, CRUISE READING WAS 1.3, ENGINE PARAMETERS NORMAL. OTHER INDICATION WAS AUDIBLE NOISE AND VIBRATION FOLLOWING THRUST CHANGE. CLEANED AND INSPECTED HOLD OPEN RODS FOR FAN COWL IAW B767 MM 77-11-10-2. VIBRATION LEVELS WERE FOUND TO BE WITHIN LIMITS PER ABX INFLIGHT AIRBORNE VIBRATION MONITORING GUIDELINE FOR B767/6E, CF680A ENGINE DATED 03/27/2001.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 37,543 hrs · 34,820 cycles

THE RIGHT HYDRAULIC QUANTITY WAS NOTED TO HAVE DECREASED TO 0.14. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC PRESSURE LINE TO THE LEFT OUTBOARD AILERON ACTUATOR IAW 767 MM 27-11-73.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 37,366 hrs · 34,757 cycles

THE RIGHT MAIN LANDING GEAR DOWN INDICATOR WAS NOTED TO BE INOPERATIVE DURING APPROACH. THE FLIGHT CREW COMPLIED WITH ABNORMAL PROCEDURES AND REPLACED THE INDICATOR BULB AS REQUIRED. THE LANDING GEAR WAS RECYCLED AND THE AIRCRAFT LANDED WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE INDICATOR LAMPS AND COMPLETED OPERATIONAL CHECKS.