N702AX

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,174 hrs · 20,812 cycles

FUSELAGE SKIN CRACKED STA 1654.5 BETWEEN STRINGER 4 LEFT AND STRINGER 5 LEFT, 3 EACH CRACKS, LONGEST CRACK 1 5/16". REPAIRED FUSELAGE SKIN CRACK AT STA 1654.5.

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,670 hrs · 20,521 cycles

EMERGENCY EXIT LIGHTS FADED OUT DURING TEST. SWITCHED BATTERY WITH SPARE IAW B767 MM 33-51-07. THE SPARE EMERGENCY LIGHT BATTERY WAS DEFERRED 56859 FOR MAINTENANCE TRACKING IAW ABX GMM 01.07.04. CLEARED DI 56859, REMOVED AND REPLACED SPARE EMERGENCY LIGHT BATTERY IAW B767 MM. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 81,798 hrs · 20,019 cycles

STANDBY EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED STANDBY EMERGENCY LIGHT BATTERY IAW B767 MM 33-51-07. OPS CHECKED GOOD.

Part: ENGINE — SURGES (RIGHT) · airframe 81,360 hrs · 19,826 cycles

RIGHT ENGINE SURGE AT CONSTANT THRUST. ENGINE WAS SHUTDOWN DUE TO UNRECOVERABLE SURGE. COMPLIED WITH/W NR 2 ENGINE INSPECTION IAW FIM 71-05-00. BOROSCOPED NR 2 ENGINE. NO DEFECTS FOUND. TURNED VSV SCHEDULE RATE SCREW ON TURN CLOCKWISE. OPS CHECK GOOD ON GROUND RUN.

Part: SLIDE — MALFUNCTIONED (PAX DOOR) · airframe 80,133 hrs · 19,340 cycles

MAIN ENTRY DOOR SLIDE WOULD NOT ARM. CYCLED MAIN ENTRY DOOR SEVERAL CYCLES. SLIDE ARM MECHANISM ARMED AND DISARMED AS REQUIRED. ALL CHECKS GOOD IAW B767 AMM.

Part: GIRT BAR — CONTAMINATED (PAX DOOR SLIDE) · airframe 80,113 hrs · 19,332 cycles

CREW REPORTED MAIN ENTRY DOOR SLIDE WOULD NOT ARM. CHECKED FOR DEBRIS IN GIRT BAR AREA. CLEARED AREA AND CYCLED DOOR. DOOR CHECKED GOOD. SLIDE ARMS AND DISARMS.

Part: GIRT BAR — FAILED (ESCAPE SLIDE) · airframe 79,758 hrs · 19,192 cycles

LT FORWARD ENTRY DOOR GIRT BAR FAILED TO LOCK. PLACED MED EMERGENCY ESCAPE SLIDE ON DEFERRAL AND MAINTENANCE PROCEDURES COMPLIED WITH. CLEARED DEFERRAL. FOUND SEAL ON LOWER FORWARD BUSTLE BINDING. TRIMMED SEAL ON BUSTLE AND EMERGENCY SLIDE ARMS NORMAL IAW B767 MM 25-66-05.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 79,502 hrs · 19,101 cycles

EMERGENCY DECLARED. AIR DIVERSION FROM ILN TO ORD, FLIGHT 1408. RIGHT PACK INOP AND PACK OFF LIGHT ILLUMINATED. EICAS MESSAGE'S RIGHT PACK OFF AND RIGHT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STANDBY SELECTED OR WHEN PACK SELECTED OFF. INSPECTED RIGHT PACK FLOW CONTROL AND SHUT-OFF VALVE. INSPECTED AND CLEARED CANNON PLUG FOR SHUT-OFF VALVE. NO DEFECTS NOTED. PERFORMED OPS CHECK OF RIGHT PACK SYSTEM. OPS CHECKED GOOD. SUSPECT ICE IN INLET DOOR. NO FAULTS. PLACARD REMOVED.

Part: PRESSURE SWITCH — DEFECTIVE (LT ENGINE OIL) · airframe 78,414 hrs · 18,676 cycles

LT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED & ENG SHUTDOWN. NR 1 ENG OIL PRESSURE LIGHT DID NOT COME ON. C/W FIM 79A-35-00-90, OIL FILTER EICAS MESSAGE WAS NOT DISPLAYED AT AIRCRAFT ARRIVAL THOUGH ENGINE WAS STILL WINDMILLING IN HEADWIND. EXAMINED NR 1 ENGINE OIL STRAINER, NO CONTAMINATION. REPLACED NR 1 ENGINE MAIN OIL SCREEN. EXAMINED THE FULL FLOW MASTER CHIP DETECTOR FOR CONTAMINATION, NONE NOTED. INSPECTED ALL ENGINE AND GEARBOX CHIP DETECTORS WITH NO CONTAMINATION NOTED IAW AMM. C/W ENGINE RUN, NO DEFECTS ON ENGINE RUN AFTER NR 1 FILTER CHANGE. REPLACED DIFFERENTIAL OIL PRESSURE SWITCH ON NR 1 ENGINE. PERFORMED ADJ TEST OF OIL BYPASS WARNING SYSTEM. CHECKED GOOD.

Part: SPRING — FAILED (ESCAPE SLIDE) · airframe 78,284 hrs · 18,637 cycles

MAIN ENTRY DOOR ESCAPE SLIDE DEPLOYMENT BAR WOULD NOT STAY UP. REPLACED DEPLOYMENT BAR GAS SPRINGS. OPS CHECKED GOOD IAW B767 AMM 26-66-01.

Part: ELEMENT — DEFECTIVE (COCKPIT WINDOW) · airframe 77,602 hrs · 18,403 cycles

CREW DETECTED A BURNING ELECTRICAL ODOR IN THE COCKPIT AFTER TAKEOFF. THE PROBABLE SOURCE WAS LOCATED BY OBSERVING A DISCOLORED/CHARRED AREA OF THE RT FORWARD WINDOW. LOWER RIGHT CORNER WHERE THE ELECTRICAL WIRING CONNECTS TO THE WINDOW HEAT ELEMENT. RIGHT FORWARD WINDOW HEAT SWITCH WAS SELECTED TO OFF AND ODOR DISSIPATED. REPLACED R1 WINDOW IAW B767 AMM 56-11-01-4. REPLACED TERMINAL LEAD TO THE WINDOW HEAT. OPS CHECKED GOOD IAW B767 MM 30-41-00-5.

Part: ODOR — DETECTED (COCKPIT) · airframe 77,593 hrs · 18,401 cycles

UNUSUAL ODOR IN COCKPIT. STRONGEST IN FOOT WELLS. NO NOTICABLE ODOR AFT OF COCKPIT DOOR. RAN APU AND PACKS, STILL NO ODOR. INSPECTED COCKPIT AND FOUND NOTHING OUT OF ORDINARY.

Part: BOLT — BROKEN (RT WING SPAR) · airframe 77,133 hrs · 18,245 cycles

RIGHT MAIN LANDING GEAR ACTUATOR ATTACH FITTING AT REAR SPAR AREA HAD BROKEN BOLT HEADS, 2 EACH, AT AFT AND FRONT OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED FASTENERS AT REAR SPAR IAW BOEING SRM 51-00-00.

Part: PRESSURE SWITCH — DEFECTIVE (ENGINE OIL) · airframe 75,709 hrs · 17,745 cycles

LT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. NOTE: LT ENGINE SHUTDOWN, (0) OIL PRESSURE LAST 5 MINUTES OF FLT. REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL FILTER AND THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH IAW MM. LEAK AND OPS CHECKED GOOD.

Part: SWITCH — DEFECTIVE (#1 ENGINE) · airframe 73,980 hrs · 17,156 cycles

LEFT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. #1 ENGINE SHUTDOWN, EMERGENCY DECLARED, DIVERTED TO SLC. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. REPLACED THE OIL PRESSURE SWITCH ON THE LEFT ENGINE. SYSTEM OPS CHECKED GOOD IAW BOEING MM.

Part: LINE — RUPTURED · airframe 73,204 hrs · 16,918 cycles

"C" HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO, AND THE SYSTEM PRESSURE AND QUANTITY LIGHTS ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED HYDRAULIC LINE P/N AS115-10K0324. THE SYSTEM WAS SERVICED AND ALL FLIGHT CONTROLS WERE CYCLED SEVERAL TIMES. OPERATION AND LEAK CHECKS WERE SATISFACTORY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,162 hrs · 16,906 cycles

GOUGE/DENT IN RIGHT AFT FUSELAGE, TEN FEET AFT OF PIT APPROXIMATELY 11 INCHES IN LENGTH. REPAIRED DAMAGED SKIN BELOW RIGHT SERVICE DOOR, AFT LOWER CARGO DOOR AS REQUIRED IAW REA B653-42263-MR AND B767 SRM 53-00-01.

Part: COMPUTER — FAULTY (ELEVATOR) · airframe 73,120 hrs · 16,889 cycles

CREW REPORTED ELEVATOR CONTROL SURFACE PRESSURE MUCH HIGHER THAN NORMAL. AIRCRAFT WAS DIFFICULT TO ROTATE ON TAKEOFF. A VIBRATION WAS ALSO FELT IN THE CONTROL YOKE THREE TIMES ON APPROACH TO ILN. REPLACED THE ELEVATOR FEEL COMPUTER IAW B767 AMM 27-31-19-4. ADJUSTED ELEVATOR BODY CABLES IAW B767 AMM 27-31-00-5. EVALUATION FLIGHT SATISFACTORY.

Part: SLIDE — DEPLOYED (CABIN) · airframe 73,003 hrs · 16,850 cycles

THE CREW INADVERTANTLY DEPLOYED THE EMERGENCY ESCAPE SLIDE. NO SLIDE INFLATION. REPLACED THE MAIN ENTRY DOOR SLIDE IAW B767 MM 25-66-00.