N611FX

ATA 2530

Part: MICROWAVE OVEN — ODOR (ZONE 900) · airframe 1,852 hrs · 1,070 cycles

DIVERTED DUE TO A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT DURING CRUISE, ISOLATED TO THE GALLEY MICROWAVE OVERHEATING. THE CREW DISCONTINUED MICROWAVE USE AND DIVERTED TO LIML. AIRCRAFT LANDED WITHOUT INCIDENT AT LIML. REPLACED MICROWAVE IAW AMM 25-32-02. TESTED SATISFACTORY.

ATA 3240

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 6,571 hrs · 5,285 cycles

AT GEAR DOWN WITH AUX HYD PUMP ON & FLAPS 20, NORMAL BRAKE FAILED RED CAS ILLUMINATED. RAN THE CHECKLIST & CONTINUED WITH A BRAKE FAULT WHITE CAS. ON LANDING WE HAD NO BRAKES. USED EMER PARKING BRAKE FOR LANDING & TAXI.

ATA 3610

Part: CLAMP — OUT OF POSITION (RT NACELLE) · airframe 3,358 hrs · 2,689 cycles

RIGHT ENG PYLON OVERHEAT CAS. AIR DIVERSION WITH UNEVENTFUL LANDING AND TAXI. CREW REQUESTED THE FIRE TRUCKS TO BE ROLLED BUT NO EMERGENCY WAS DECLARED. REPOSITIONED LP AND HP CLAMPS. SATISFACTORY LEAK CHECK PERFORMED. INSTALLED 2 NEW TEMP STRIPS AT HP AREA. MX FUNCTIONAL CHECK FLIGHT SATISFACTORY.

ATA 3260

Part: POSITION SWITCH — FAILED (ACTUATOR) · airframe 2,592 hrs · 2,044 cycles

RETRACTED MLG AND THE WHITE AND BLACK HASH MARK INDICATORS INDICATING THE GEAR DOORS WERE OPEN ILLUMINATED. RECYCLED THE GEAR AND THE RESULT WAS NOSE GEAR DOWN AND LOCKED AND THE MAIN'S RETRACTED. CREW EXTENDED THE GEAR AND ALL GEAR INDICATIONS SHOWED 3 GREEN DOWN AND LOCKED. CREW PERFORMED AN AIR RETURN, WITH UNEVENTFUL LANDING AND TAXI. MX REPLACED RT MAIN INBD DOOR ACTUATOR (CONTAINS THE INTERNAL POSITION SWITCH). LEAKS AND OPS CHECK GOOD.

ATA 7797

Part: WIRE HARNESS — DAMAGED · airframe 1,317 hrs · 997 cycles

LEFT ITT IRRATIC DURING FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. LEFT ITT IRRATIC DURING FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. EMERGENCY DECLARED FOR LANDING. PILOT REPORTED THAT THE LEFT ITT EXCEEDED 1014* TWICE AND THE PILOT PERFORMED AN IN-FLIGHT SHUTDOWN. BOTH N1 INDICATIONS WERE MATCHED. BOTH FF INDICATIONS WERE MATCHED. PILOT FURTHER REPORTED THAT THE LEFT ITT INDICATION FOLLOWING ENGINE SHUTDOWN WAS 940* AND REMAINED SO UNTIL TOUCHDOWN. MX REVIEWED THE ECTM DOWNLOAD AND THE DEEC SAW THE ITT OUT OF RANGE. RECOMMENDED REPLACING THE ENGINE HARNESS PART NUMBER 3060757-1 OR -2. ENGINE HARNESS REPLACED AND GROUND POWER RUNS PERFORMED. NO FURTHER DEFECTS NOTED.

ATA 7797

Part: WIRE HARNESS — UNKNOWN (ITT INDICATOR) · airframe 1,317 hrs · 997 cycles

PILOT REPORTED THAT THE LT ITT EXCEEDED 1014 DEGREES TWICE AND THE PILOT PERFORMED AN IN-FLIGHT SHUTDOWN. BOTH N1 INDICATIONS WERE MATCHED. BOTH FF INDICATIONS WERE MATCHED. PILOT FURTHER REPORTED THAT THE LT ITT INDICATION FOLLOWING ENGINE SHUTDOWN WAS 940 DEGREES AND REMAINED SO UNTIL TOUCHDOWN. MX REVIEWED THE ECTM DOWNLOAD AND THE DEEC SAW THE ITT OUT OF RANGE. HE RECOMMENDS REPLACING THE ENGINE HARNESS PN 3060757-1 OR -2. ENGINE HARNESS REPLACED AND GROUND POWER RUNS PERFORMED. NO FURTHER DEFECTS NOTED.

ATA 7200

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 447 hrs · 298 cycles

CREW OBSERVED THE RT ENGINE ITT INDICATION SPIKE ABOVE ALLOWED MARGIN. PERFORMED ENGINE SHUTDOWN. RESTART PERFORMED AND ENGINE PERFORMED NORMAL FOR DURATION OF FLIGHT. MAINTENANCE DOWNLOADED THE DEEC'S AND DATA SHOWED NORMAL FOR BOTH ENGINES. DAU UNITS WERE SWAPPED AND ENGINE RUNS PERFORMED WITH NO DEFECTS NOTED. PER THE TFE 731 LMM THE ENGINE RUNS SHEETS PROVED THE ENGINE OPERATING UNDER NORMAL PARAMETERS. AIRCRAFT RETURNED TO SERVICE AND WILL BE MONITORED FOR FURTHER OCCURANCE. THIS DATA HAS BEEN FORWARDED TO LEARJET ENGINEERING VIA THE JSLLC CAS REPORTING SYSTEM.

ATA 2761

Part: ACTUATOR — FAILED (SPOILER) · airframe 399 hrs · 261 cycles

SPOILER FAIL CAS ILLUMINATED ON TAKEOFF ROLL THEN WENT OUT WHEN SPOILERS DEPLOYED. MAINTENANCE INTERROGATED THE MCOS COMPUTER AND FOUND SPOILERS FAILED ON RETRACT, GO CODE 2428 LR ACTUATOR COMMAND DOES NOT MATCH ACTUATOR POSITIONS. MX RANG THE WIRES AND FOUND THE LT ACTUATOR READINGS ARE A-B IS 706 OHMS, A-C IS 354, B-C IS 352 OHMS. ON THE RT SIDE A-B IS 648 OHMS, A-C IS 343, AND B-C IS 342 OHMS. FSR RECOMMENDS REPLACEMENT OF THE SPOILER ACTUATORS. ACTUATORS REPLACED IAW AMM AND GROUND CHECKS PERFORMED. NO ADDITIONAL DISCREPANCIES NOTED. THIS DATA HAS BEEN FORWARDED TO MFG ENGINEERING THROUGH THE JSLLC CAS REPORTING SYSTEM.