N719QS

ATA 2797

Part: CIRCUIT BOARD — FAILED (COCKPIT) · airframe 5,920 hrs · 3,814 cycles

ELECTRICAL BURNING ODOR OBSERVED BY BOTH CREW DURING FLIGHT. COFFEE HEATERS WERE TURNED OFF & ODOR REMAINED. LT & RT GEN SHOWED 170 & 130 AMP, SPLIT RESPECTIVELY & WERE FLUCTUATING +/- 20 AMPS RAPIDLY. WHEN GALLEY & CABIN POWER WAS REMOVED AMP LOAD SEEMED TO STABILIZE. ODOR WAS STILL PRESENT INTERMITTENTLY THROUGH LANDING. R & R PCB 82P. OPS CHECKED GOOD IAW MM 21-21-00, 29-10-20, 30-10-10, 30-40-00, 33-10-10, 71-00-00 & 78-30-00. PERFORMED GENERATOR OPS TESTED IAW MM 24-30-00 & FOUND AMP SPLIT TO BE WITHIN ALLOWABLE LIMITS.

ATA 3230

Part: LANDING GEAR — UNKNOWN (MAINS) · airframe 4,996 hrs · 3,232 cycles

DURING MAIN GEAR RETRACTION, FIRST MOVEMENT OF GEAR HANDLE FROM FULL DOWN TO FULL UP, AN ABNORMAL LOUD BANG WAS HEARD COMING FROM THE LOWER FUSELAGE FWD TO CENTER SECTION. RETRACTION SEQUENCE COMPLETELY NORMAL WITH NO ABNORMAL MESSAGES OR INDICATIONS. GEAR EXTENSION ON LANDING WAS NORMAL. PERFORMED DETAILED INSPECTION OF NOSE AND MAIN LANDING GEAR ASSEMBLIES. NO DEFECTS NOTED. PERFORMED LANDING GEAR EXTENSION AND RETRACTION NUMEROUS TIMES WITH NO ABNORMAL SOUNDS OR DISCREPANCIES NOTED. WORK PERFORMED IAW G200 AMM 32-30-00.

ATA 7200

Part: ENGINE — SHUTDOWN (LEFT) · airframe 4,374 hrs · 2,851 cycles

10 MINUTES AFTER DEPARTURE, LEFT ENGINE SHUTDOWN INFLIGHT, CLIMBING THROUGH 12,400 THE LT FADEC FAULTY ICAS ILLUMINATED. LT N2 INDICATOR TURNED RED BRIEFLY AND THE ITT HAD A 100 DEGREE SPLIT (L750/R850). 10-15 SECONDS LATER THE LT ENGINE SHUTDOWN. LT ENGINE WINDMILLED ABOUT 20 MIN. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE.

ATA 3240

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 4,222 hrs · 2,731 cycles

BRAKES REQUIRE EXCESSIVE PRESSURE TO ACTIVATE, WHEN THEY DO ACTIVATE THEY GRAB THEN FADE TO A HARD PEDAL WITH LITTLE BRAKING ACTION. DUPLICATED DISCREPANCY DURING TAXI CHECK & FOUND AIR TO BE IN BRAKE SYS. PROCEDED TO PERFORM BRAKE BLEEDING ACTIONS IAW MM 32-40-20 PERFORMED TAXI CHECK. OPS CHECK OF BRAKES OK.

ATA 3230

Part: LANDING GEAR — MALFUNCTIONED (RT MAIN) · airframe 4,162 hrs · 2,691 cycles

AFTER TAKEOFF, WITH NORMAL MLG RETRACTION, RT MLG RED CROSS HATCH UNSAFE LIGHT ILLUMINATED. LT MLG AND NLG RETRACTED NORMALLY. DEPARTED AIRFIELD WITH SNOW ON TAXI WAYS. DELAYED MLG RETRACTION AFTER TAKEOFF WITH RESPECT TO FIELD CONDITIONS. COMPLETED MLG DOES NOT LOCK UP CHECKLIST, CONDITION REMAINED. MLG EXTENSION NORMAL. COULD NOT DUPLICATE.

ATA 2120

Part: UNKNOWN — ODOR (CABIN) · airframe 3,452 hrs · 2,234 cycles

AFTER TAKEOFF ELECTRICAL ODOR IN CABIN. AFTER TURNING OFF CABIN/ GALLEY POWER NO CHANGE. NOTICED LIGHT HAZE IN CABIN MOVING FORWARD. SELECTED ECS TO RT, THEN LT NO CHANGES. SELECTED ECS RAM AND HAZE CLEARED. RAN ENGINES AT MAX CRUISE POWER FOR 20 MINUTES EA WITH NO ODOR OR HAZING NOTICED. INSPECTED ECU & PLUMBING WITH NO FAULTS FOUND. INSPECTED & REPLACED BOTH OIL FILTERS WITH NEW. WO 39916 FOR FURTHER INSPECTIONS PERFORMED. ALL WORK DONE IAW MM 29-20-05. OPS & LEAK CHECKED GOOD.

ATA 3240

Part: CONTROL VALVE — MALFUNCTIONED (ANTI SKID SYS) · airframe 2,988 hrs · 1,898 cycles

RT BRAKE GRABS SEVERELY ON LANDING. TROUBLESHOOTING OF THE BRAKE SYS REVEALED THAT THE LT ANTISKID WAS NOT ALLOWING ANY PRESSURE TO THE LT BRAKES AND THE RIGHT ANTISKID VALVE WOULD NOT MODULATE PRESSURE. REMOVED LT ANTISKID VALVE AND INSTALLED A NEW ANTISKID VALVE. OPS TESTED GOOD WITH NO DEFECTS NOTED.

ATA 3897

Part: CONNECTOR — BURNED (LAVATORY) · airframe 2,869 hrs · 1,814 cycles

WHILE TROUBLESHOOTING FLIGHT PHONE FOUND LAV PLUG 548 P2 SHOWING SIGNS OF DISCOLORATION AND OVERHEAT. CAPPED AND STOWED WIRES FOR PLUG 548 P2 IAW WDM 20-00-00 COLLARED CB'S LAV WATER HEATER, RIBBON HEATER, WATER SYS CONT, TOILET CB. VERIFIED NO POWER AT PLUGS 548 P2 & J2. INSTALLED NEW CONNECTOR. REMOVED COLLAR'S FROM LAV WATER HEATER, RIBBON HEATER, WATER SYS CONT, AND TOILET CIRCUIT BREAKERS. SYS OPS CHECKED GOOD. WORK DONE IAW DWG GA216960010, REV A.

ATA 2397

Part: CONNECTOR — DAMAGED (SATCOM) · airframe 2,801 hrs · 1,765 cycles

ON DEPARTURE, AT ABOUT 2000 FT, DETECTED AN ELECTRICAL ODOR. CHECKED THE ELECTRICAL PAGE AND THE VOLTS AND AMPS WERE NORMAL. POWERED UP ACFT AND LET RUN A HOUR. FOUND 60HZ SYS OPERATED NORMALLY. FOUND THE SATCOM HEADSET DISCONNECTED. REPAIRED CONNECTIONS, OPS CHECKED GOOD. NO ELECTRICAL ODOR NOTED. RAN ENGINE APU FOR SEVERAL MINUTES WITH NO ODOR DETECTED, ALL SYS OPERATED NORMAL AT THIS TIME.

ATA 3160

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 620 hrs · 370 cycles

CO-PILOT'S MFD WENT IN-OP IN FLT WITH A BURNING SMELL. REMOVED DISPLAY & INSTALLED PER CMP 342304 GAC SAV W/O 142032 SQUAWK 6.1 OPS CHECK GOOD NO DEFECTS NOTED.

ATA 2210

Part: AUTOPILOT SYS — FAILED (PITCH) · airframe 534 hrs · 321 cycles

AUTO PILOT PITCH FAILED. PERFORMED HORIZONTAL STABILIZER TRIM SYSTEM INTERFERENCE TEST, TRAVEL TEST, AND FUNCTIONAL TEST I.A.W. G200 M.M. 27-40-00. OPS CHECK GOOD.