N429EM

BEECH B200 · 1985 · Valid Registration

Registered owner: EAGLEMED LLC, KS (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
EAGLEMED, LLC (7EMA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

P · 2017-07-31 Matched by certificate designator
ATA 3260

NO RIGHT MAIN LANDING GEAR DOWN AND LOCK INDICATION. FOUND BURNED OUT LIGHT BULB.

Source: SDR 7EMA201708010001 · FAA SDRS
F · 2012-08-08 Matched by certificate designator
ATA 7321

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.

Source: SDR 7EMA20120808429 · FAA SDRS
O · 2012-08-06 Matched by certificate designator
ATA 7603

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,

Source: SDR 7EMA20120806429 · FAA SDRS
O · 2010-06-08 Matched by certificate designator
ATA 2130

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.

Source: SDR IJAA2010061000001 · FAA SDRS
B · 2010-03-15 Matched by certificate designator
ATA 2497

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-PILOT’S 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.

Source: SDR IJAA2010031600001 · FAA SDRS