1978 Beech T-34C-1 Turbo Mentor
s/n GM56 N94GR
This Aircraft is in Standard Category with no Spar A.D.'s
Specifications
Airframe: 11,352.2 TTSN
216.2 SMOH
Engine: Pratt & Whitney PT6A-25 (550 shp) equipped for inverted flight.
29.2 since IRAN by Covington Engines
Propeller: Hartzell 3 bladed Propeller: 29.2 hrs SPOH w/ new blades
Avionics: Collins Radios with Stratus ESG ADS-B Transponder
Annual: 4/2020
29.2 hours since assembly and inspection for Standard Airworthiness.
*To be able to be sure of times remaining on life limited parts the following were overhauled:
*Flap Motor
*Flap Actuators
*Gear Motor
*Landing Gear Gearbox
*New Wing Bolts
*Hartzell Propeller
*Prop Governor
*Overspeed Governor
*Torque Gauge
*ITT Gauge
*New Airspeeds reflecting civilian limitations.
*Landing gear was disassembled and stripped for NDT testing, then primed/painted and reassembled using all new hardware.
Lots of routine maintenance was accomplished but lots of details were taken care of during assembly in anticipation of paint and panel upgrades, to include:
*New Canopies
*New Flap Cables
*New 406 ELT
*New seat cushions installed.
*Engine was sent to Covington for an IRAN as part of the assemble process.
*All new hardware in empennage, wings, and flight controls.
*Wheel wells stripped and painted before reassembly.
*New Tires, Bearings, and Brakes at this time.
*New weight and balance done at this time.
Performance:
*190 kts tas
*32 gph
*1,500 fpm climb
*500 nm legs are very conservative
*2900# Empty Weight
*4300# Gross Weight
