N429EM
Registered owner: EAGLEMED LLC, KS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| EagleMed, LLC (7EMA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
5 reports on file, 2010-03-15 – 2017-07-31.
Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 11,030 hrs · 11,976 cycles
NO RIGHT MAIN LANDING GEAR DOWN AND LOCK INDICATION. FOUND BURNED OUT LIGHT BULB.
Part: FUEL CONTROL — INOPERATIVE (RT ENGINE) · airframe 7,427 hrs · 7,497 cycles
ON DECENT, THE RT ENGINE FAILED TO RESPOND TO POWER LEVER MOVEMENT, TORQUE REMAINED AT 2000 LBS. AFTER TRYING SEVERAL TIMES TO GET RT ENGINE TO RESPOND BY MOVING POWER LEVER FORWARD AND AFT, ENGINE WAS SECURED, DECLARED EMERGENCY AND MADE SAFE LANDING. REMOVED FUEL CONTROL AND INSTALLED SERVICEABLE. RIGGED ENGINE, OPS AND LEAK CHECKS GOOD. ACFT IS APPROVED FOR RETURN TO SERVICE.
Part: LINKAGE — DIRTY (POWER LEVER) · airframe 7,424 hrs · 7,493 cycles
ON DESCENT, THE RT ENGINE FAILED TO RESPOND TO POWER-LEVER MOVEMENT, TORQUE REMAINED AT 2000 LBS. AFTER TRYING SEVERAL TIMES TO GET RT ENGINE TO RESPOND BY MOVING POWER LEVER FORWARD AND AFT, ENGINE WAS SECURED, DECLARED EMERGENCY AND MADE SAFE LANDING. MX CONTACTED AND INVESTIGATED PROBLEM. FOUND LINKAGE TO BE DIRTY. CLEANED LINKAGE. OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE,
Part: SOLENOID VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 6,045 hrs · 5,475 cycles
AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. PERFORMED AIRTURN BACK TO AIRPORT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE SAFETY SOLENOID VALVE. AIRCRAFT SYSTEM TEST AND FLIGHT CHECK SATISFACTORY.
Part: BUSS BAR — SHORTED (C/B PANEL) · airframe 5,884 hrs · 5,324 cycles
PILOT REPORT OF SPARKS AND SMOKE FROM CO-PILOT'S CIRCUT BREAKER PANEL AND LOSS OF NR1 COMM, NR 1 NAV AND SATCOM. INSPECTED AND FOUND ADEL CLAMP LOCATED BEHIND CO-PILOTâS CIRCUIT BREAKER PANEL SHORTING AGAINST NR1 BUS BAR. REPOSITIONED ADEL CLAMP, REPLACED AVIONICS BUS NR 1 FEEDER LIMITER AND PERFORMED A CHECK OF NR 1 AND NR 2 COMS, NAVS, AND SATCOM SYS. ALL CHECKS SATISFACTORY.