Yakovlev Yak 52 — yak52_fltrep52 NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full Source: Yakovlev/Yak 52/yak52_fltrep52.txt Rights: licensed Checklist hash: 0f28b1a9f2d5130aba7a6dcd55653cced8366193b967dd41ac34fcfede2fdddb Verify against the aircraft's own approved documentation before use. ======================================================================== COCKPIT ENTRY ------------- [ ] Climb onto wing using knee, then other leg, while holding canopy rail [ ] Walk only on anti-skid strip adjacent to fuselage BEFORE START ------------ [ ] Check front cockpit wall chart for priming duration [ ] Check air reservoir pressure ** NOTE: Air reservoir is good for 12 start attempts before re-charging. ENGINE START ------------ [ ] Start using pneumatic system ** NOTE: Starting procedure varies with outside air temperature, time since last run, and oil dilution. ** NOTE: When warm, the Ivchenko starts with the simplicity of a typical Continental or Lycoming. AFTER START ----------- [ ] Check compressor re-charges air bottle after start TAXI ---- [ ] Use rudder bars for gentle turns [ ] Use burst of power to energize rudder when needed [ ] For tighter turns, use full rudder plus stick-mounted brake lever for differential braking ** NOTE: With rudders neutral, braking is equal to both main wheels. ** CAUTION: Take care not to reach excessive taxi speed; allow engine temperature to stabilize. ENGINE RUN-UP AND VITAL ACTIONS ------------------------------- [ ] Magnetos check [ ] Exercise RPM control to verify propeller governor operation [ ] Complete pre-takeoff vital actions using checklist ** NOTE: Max power (ceaseless engine function duration) is 5 minutes. ** NOTE: Throttle-engine lag (racing capacity) is 3 seconds max. ** NOTE: Max overspeed when operating throttle rapidly is 109 per cent. ** NOTE: Maximum allowed airspeed in level flight is conditioned by avoidance of sudden spin: 130 km/h normal flight, 170 km/h inverted. Author suspects max/min are reversed. ** CAUTION: Aerobatics forbidden with less than 4.5 gallons of fuel remaining. TAKEOFF ------- [ ] Apply full throttle [ ] Expect to push on the 'wrong' foot due to engine rotation direction [ ] Rotate ............................................. 120 km/h (65 kt) ** NOTE: Take-off roll in ISA conditions is 590 ft at maximum weight. AFTER TAKEOFF ------------- [ ] Raise gear .................................. BELOW 200 km/h (108 kt) [ ] After selecting gear up, hold lever until 'three reds', then return lever to neutral CIRCUIT AND APPROACH -------------------- [ ] Lower gear ..................................... AT 200 km/h (108 kt) [ ] After selecting gear down, hold lever until 'three greens', then return lever to neutral [ ] Extend flaps ........................... AT/OR BELOW 170 km/h (92 kt) [ ] Fly approach ... 170 km/h (92 kt) slowing to 120 km/h (65 kt) at threshold ** NOTE: Without flaps, forward view from rear seat is virtually nil; a curved approach is needed. LANDING ------- [ ] Keep the canopy lock pin in place in the rail hole [ ] Lower nose after touchdown ** NOTE: High wing-loading means no tendency to float. ** NOTE: With practice, landing roll can be as short as 300 m (985 ft). FORCED LANDING -------------- [ ] Leave gear retracted for dead-stick landing ** NOTE: Standard drill is to leave gear retracted to flatten the descent profile. ** NOTE: Brakes remain usable with gear up. ** NOTE: With gear up, the undercarriage remains partially exposed to minimize damage in a wheels-up landing. REFERENCE --------- ** NOTE: Performance: climb to 3,000 ft in 98 seconds; cruise 140-145 kt at 75 per cent power; fuel burn just over 13 US gal/hr at 140 kt cruise. ** NOTE: Endurance in excess of 2 hours with 45 minutes reserve; maximum range 275 nm at slightly reduced cruise speed. ** NOTE: G limits: unlimited aerobatics certified at max takeoff weight 1,305 kg. ** NOTE: Engine: Ivchenko M-14P 9-cylinder radial, 360 hp. ** NOTE: Pneumatic system used for engine starting, flaps, gear, and brakes. ** NOTE: RPM gauge is calibrated in percent of maximum rather than RPM. ** NOTE: Artificial horizon is inverted in presentation: top half of ball is brown, bottom half is blue. ** NOTE: Rear cockpit has controls to deliberately fail certain systems in the front cockpit. ** NOTE: Gear lever is pneumatic and returns to central neutral position when not required. ** NOTE: Brakes are operated by a stick-mounted lever; pneumatic brake noise resembles a bus/lorry stopping.