N710QS

ATA 7930

Part: ANNUNCIATOR — INOPERATIVE (ENGINE OIL) · airframe 4,849 hrs · 3,740 cycles

UPON ADVANCING POWER FOR T/O, ENGINE OIL PRESSURE WARNING LIGHT CAME ON. TAPES FOR TEMP AND PRESSURE INDICATED NORMAL. INSTALLED REPAIRED ANNUNCIATOR PANEL IAW CESSNA 650 MM CHAP 31-10-01, OPS CHECK GOOD.

ATA 3241

Part: DISCONNECT UNIT — CORRODED (BRAKES) · airframe 4,658 hrs · 3,574 cycles

BRAKES FADED ON ROLLOUT, TURNED ANTI-SKID OFF BRAKES WORKED NORMAL. BRAKES WOULD NOT HOLD DURING STATIC THRUST CK ABOVE 61 PERCENT N1, WITH ANTI SKID ON. ANTI SKID OFF BRAKES ARE NORMAL. REMOVED AND REPLACED CORRODED RT WHEEL WELL CONNECTOR JW18 IAW 650 WM CHP 32-40-01. ANTI-SKID SYSTEM OPS CK'D GOOD IAW 650 MM CHP 32-42-00. REMOVED LEFT AND RIGHT INBOARD MAIN TIRE DUE TO TIRES FLAT. INSTALLED NEW LEFT AND RIGHT INBOARD MAIN TIRES IAW CE650 M/M CH 32-41-02.

ATA 3260

Part: SQUAT SWITCH — INTERMITTENT (MLG) · airframe 4,567 hrs · 3,509 cycles

DURING ROLL OUT (AT APPROXIMATELY 20 - 30 KNOTS) THE BRAKES RELEASED EVEN THOUGH THE BRAKING PRESSURE WAS NOT REDUCED. THE AIRPLANE CONTINUED ROLLING FOR APPROXIMATELY 15-30 YARDS THEN THE BRAKES KICKED BACK IN AGAIN. TROUBLESHOT BRAKE CONTROL SYSTEM, FOUND INTERMITTANT RIGHT HAND SQWAT SWITCH. REMOVED THE RIGHT SQWAT SWITCH AND REPLACED WITH A NEW SWITCH AND INSTALLED A NEW CONNECTOR P/N MS27473T10F98P. ALL WORK PERFORMED IAW CE-650 MM CH 32-60-00 AND WIRING MANUAL CH 20-00-00. OPS CHECK SATISFACTORY.

ATA 2612

Part: FIRE DETECTOR — MALFUNCTIONED (APU BAY) · airframe 4,395 hrs · 3,377 cycles

APU FIRELIGHT CAME ON IN FLIGHT, PUSH THE LIGHT AND BLEW THE BOTTLE AS PER CHECKLIST, INSPECTED APU AND SURROUNDING AREA NO DAMAGE NOTED, MEL PER CE-650 NJA MEL MANUAL. ITEM IS UNDER INVESTIGATION.

ATA 3220

Part: LANDING GEAR — NOISY (NOSE) · airframe 4,140 hrs · 3,156 cycles

AFTER GEAR RETRACTION, AN AUDIBLE THUMP CAN BE HEARD. THIS IS COMING FROM THE NOSE GEAR AREA AND OCCURS ABOUT ONCE EVERY 30 SECONDS. ACCOMPLISHED FERRY FLIGHT INSPECTION TO BTL FOR MAINTENANCE.

ATA 3220

Part: LANDING GEAR — VIBRATION (NOSE) · airframe 4,140 hrs · 3,155 cycles

UPON NORMAL LANDING GEAR RETRACTION, NOSE GEAR WOULD RETRACT AND SOON AFTER (10 MIN) AUDIBLE BUMP WAS HEARD WITH NOTICABLE VIBRATION. APPROX 10 MIN LATER SAME SOUND & VIBRATION WAS HEARD A SECOND TIME, BUMP & VIBRATION WAS NOTED IN ALL PHASES OF FLIGHT. ITEM IS UNDER INVESTIGATION.

ATA 7200

Part: ENGINE — FLAMED OUT (LEFT) · airframe 3,336 hrs · 2,550 cycles

ON ENGINE START LEFT ENGINE FLAMED OUT AT IDLE SPEED. PERFORMED ENGINE INSPECTION FOR ENGINE FLAME OUT ON START, SUMPED WING TANKS IAW CESSNA 650 MM CHAPTER 12-10-10, INSPECTED ENGINE FUEL FILTER. CHECKED DEEC FOR FAULTS AND RUN ENGINE TO POWER IAW TFE731 MM CHAPTER 72-00-00, 73-21-02, ALL ENGINE PARAMETERS CHECKED GOOD.

ATA 3230

Part: VALVE — STUCK (MLG) · airframe 3,148 hrs · 2,402 cycles

AFTER TAKE OFF, DURING GEAR RETRACTION THE LANDING GEAR "UNLOCK" ANNUNCIATOR REMAINED ILLUMINATED, CYCLES GEAR SEVERAL TIMES LIGHT REMAINED ON, DIVERTED INTO BFI AND LANDED SAFELY. TROUBLESHOT AND FOUND RETRACT PRESSURE RELEASE VALVE STUCK. RESEATED VALVE AND ACTUATED 50 TIMES LEFT AND RIGHT NO FURTHER STICKING OR BINDING NOTED. PERFORMED 15 NORMAL GEAR CYCLES AND 5 EMERGENCY EXTENSIONS ALL CHECKED GOOD, SERVICED RESERVOIR TO FULL AND GEAR BOTTLE TO 2000 PSI REFERENCE CESSNA 650 MM CHAPTER 12-11. PERFORMED 3 MORE NORMAL GEAR CYCLES, BLED SYSTEM ALL CHECKS GOOD.

ATA 3260

Part: UPLOCK SWITCH — OUT OF ADJUST (LT MLG) · airframe 2,959 hrs · 2,245 cycles

AFTER TAKE OFF FROM ORD, DURING GEAR RETRACTION GEAR UNLOCK LIGHT STAYED ON. CYCLED GEAR BUT NO HELP. - FOUND LT UPLOCK ACTUATOR ASSEMBLY, UPLOCK SWITCH AND LT MLG CAMBER OUT OF ADJUSTMENT.