N292QS

ATA 5210

Part: CABLE — FAILED (PAX DOOR) · airframe 12,193 hrs · 7,589 cycles

MAIN CABIN ENTRY DOOR LIFT HANDLE IS BROKEN. UNABLE TO OPEN OR SHUT DOOR FROM INSIDE THE CABIN. R & R THE DOOR LIFT HANDLE CABLE IAW MM 52-40-00. PERFORMED OPS TEST IAW MM 52-10-00, OPS TESTED GOOD.

ATA 3230

Part: SWITCH — INOPERATIVE (MLG) · airframe 11,209 hrs · 6,983 cycles

AFTER TAKEOFF AND SELECTING THE GEAR HANDLE TO THE UP POSITION, THE GEAR DID NOT RETRACT. IT FELT AS THOUGH THE GEAR DOORS DID NOT OPEN. THE 3 GREEN "DOWN" LIGHTS REMAINED ON AND NONE OF THE RED "UNSAFE" LIGHTS ILLUMINATED. THE GEAR HANDLE WAS SELECTED TO THE DOWN POSITION AND THE 3 GREEN "DOWN" LIGHTS REMAINED ON. WE DID NOT RECEIVE ANY INDICATION OF A RED OR AMBER BRAKE LIGHT. THERE WERE NO RED MINELCOS INDICATING AFTER SHUTDOWN. THERE WERE NO MESSAGES INDICATING ON THE NR 2 EIED. THERE WERE NO CODES DISPLAYED ON EITHER BSCU AFTER DOWNLOADING INFORMATION FROM THE ACFT COMPUTER. TESTED RT AND LT MAIN GEAR DOOR ACTUATOR. PROX SWITCHES WITH TEST BOX AND FOUND LT DOOR ACTUATOR SWITCH FAIL TO THE DOOR OPEN POSITION. PLACED NEW SWITCH ON ORDER. RECIEVED NEW SWITCH. REPLACED FAILED SWITCH WITH NEW SWITCH. JACKED ACFT AND COMPLIED WITH 6 GEAR RETRACTIONS AND EXTENSIONS WITH NO DEFECTS NOTED, REF F2000, MM 32-31-00-860-801, 20-00-00-910-803 AND IPC 32-12-30-20.

ATA 3230

Part: PCB — FAILED (MLG) · airframe 11,186 hrs · 6,969 cycles

AFTER TAKEOFF, GEAR HANDLE SLECTED TO UP POSITION. NO GEAR SEQUENCE ACTION TOOK PLACE WITH ALL THREE GREEN INDICATIONS VISIBLE & NO RED GEAR LIGHTS. AFTER 20 SECONDS GEAR HANDLE BEGAN TO FLASH RED. FIVE SECONDS LATER, GEAR BEGAN TO SEQUENCE AUTOMATICALLY & ALL THREE GEAR RETRACTED WITH NO RED GEAR INDICATIONS. GEAR SELECTED DOWN & AFTER FIVE SECONDS, SEQUENCE BEGAN, & ALL GREEN DOWN GEAR LIGHTS DISPLAYED WITH NO RED LIGHTS. BOTH RED "STEERING" & "BRAKE" MINELCOS VISIBLE, FAULT CODES 315, STRUT PROXIMITY SWITCH FAILURE & 415, STRUT PROXIMITY SWITCH FAILURE. FAULT CODE 415 IS A REPEAT. RESEARCHED DISCREPANCY & MCC SUPPLIED HISTORY. PERFORMED ACFT MM TASK 32-30-00-720-801, NORMAL OPERATION. FUNCTIONAL TEST OF EXTENSION & RETRACTION OF LANDING GEAR AND DOORS. ABLE TO INTERMITTENTLY DUPLICATE DISCREPANCY TWO TIMES WITH 30 CYCLES OF GEAR. CHECK INPUT POWER TO V1 OF RELAY AND WAS ABLE TO DUPLICATED A EXTENDED DELAY OF POWER WHILE CYCLING GEAR HANDLE. MONITORED POWER AT 10GW-6 & GROUND AT 10GW-2, NO DEFECTS NOTED. GEAR HANDLE 100GM PREVIOSULY REPLACED, SUSPECT INTERMITTENT TIME DELAY ON 10GW. R & R PCB 10GW, IAW MM TASK 20-00-00-910-803, PERFORMED MM TASK 32-30-00-720-801-01, NORMAL OPS & FUNCTIONAL TEST OF EXTENSION & RETRACTION OF LANDING GEAR & DOORS. CYCLED GEAR 30 TIMES WITH NO FURTHER DEFECTS NOTED.

ATA 3230

Part: UPLOCK — INOPERATIVE (NLG) · airframe 74 hrs · 6,961 cycles

RAISED THE GEAR HANDLE AFTER DEPARTURE, GEAR DID NOT RETRACT. WE HEARD A LOUD GRINDING NOISE FROM THE NOSE WELL. JACKED ACFT. HOOKED UP MULE, WITH 1500 PSI, GEAR CAME UP. ALL 3 IN-TRANSIT LIGHTS REMAINED ON AND GEAR HANDLE FLASHED. CYCLED GEAR DOWN, ALL 3 GREEN LIGHTS ILLUMINATED. (EL)(DS) REMOVED PRESSURE AND NOSE GEAR STARTED TO DROP. NLG UPLOCK ASSY NOT HOLDING NLG. FOUND AMM FOR MANUAL RELEASE JAMMED AND WILL NOT MOVE. R & R NOSE GEAR UPLOCK BOX AND OPS CHECKED GOOD IAW MM 32-22-17-900-801.

ATA 5610

Part: WINDOW — CRACKED (COCKPIT) · airframe 9,590 hrs · 5,962 cycles

INNER MOST PANE OF DIRECT VISION CRACKED IN FLIGHT. CRACK IS ABOUT 20 INCHES LONG. REMOVED WINDOW AND INSTALLED NEW WINDOW. OPS CHECKED WINDOW HEAT SYS WITH NO DEFECTS. PRESSURIZED ACFT TO 4PSI AND LEAK CHECKED WINDOW WITH NO DEFECTS. ALL WORK ACCOMPLISHED REF MM 56-115.3

ATA 7200

Part: ENGINE — FAILED (LEFT) · airframe 9,029 hrs · 5,611 cycles

ON TAXI, LT ENG ROLLED BACK TO COMPLETE FAILURE. NO MESSAGES, NO POPPED C/B`S, ALL ELECTRIC, IGNITION & PNEUMATIC SWITCHES IN NORMAL POSITION. ONLY INDICATIONS WERE: FAILED ENGINE, OIL, HYD, & GEN LIGHTS ILLUMINATED. ENVIRONMENTAL CONDITIONS AT TIME WERE VERY GUSTY, WINDS IN EXCESS OF 30KTS, INSPECTED HMU RED & YELLOW BYPASS PINS. INSPECTED & REPLACED LT ENGINE FUEL FILTER. INSPECTED HMU & FADEC CONNECTORS. PERFORMED AN E13 CONNECTOR CHECK TO HMU. PERFORMED LT ENGINE STALL CHECK, & POWER ASSURANCE RUN. REPOSITIONED FADECS 1A & 2B FOR MX. PERFORMED HMU OPS TEST. DOWNLOADED FADEC'S & SENT FOR EVALUATION. ALL TESTS PASSED. DONE IAW MM 73-20-01, 72-00-00, 76-10-05, MM 71-000, 71-008.

ATA 5270

Part: CONTACT — DIRTY (DOOR) · airframe 5,060 hrs · 3,178 cycles

ON TAKEOFF ROLL, RED MASTER DOOR LIGHT CAME ON. ALL DOORS WERE CLOSED AND LOCKED. MEL'D IAW NETJETS FALCON MEL. ALL DOORS WERE OPEN & CLOSED, AND FOUND CONTACTS ON EMERGENCY EXIT DOOR TO BE DIRTY , CLEANED AND REINSTALLED DOOR AND OPS CHECK SYSTEM AND FOUND SYSTEM TO BE WORKING IAW FALCON 2000 52-700.