#	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.
section_id	phase	criticality	section_title	item_index	item_id	type	tickable	memory_item	indent	text	response	condition	detail
	preflight_inspection	normal	Cockpit Entry	0		challenge	yes	no	0	Climb onto wing using knee, then other leg, while holding canopy rail			
	preflight_inspection	normal	Cockpit Entry	1		challenge	yes	no	0	Walk only on anti-skid strip adjacent to fuselage			
	before_start	normal	Before Start	0		challenge	yes	no	0	Check front cockpit wall chart for priming duration			
	before_start	normal	Before Start	1		challenge	yes	no	0	Check air reservoir pressure			
	before_start	normal	Before Start	2		note	no	no	0	Air reservoir is good for 12 start attempts before re-charging.			
	engine_start	normal	Engine Start	0		challenge	yes	no	0	Start using pneumatic system			
	engine_start	normal	Engine Start	1		note	no	no	0	Starting procedure varies with outside air temperature, time since last run, and oil dilution.			
	engine_start	normal	Engine Start	2		note	no	no	0	When warm, the Ivchenko starts with the simplicity of a typical Continental or Lycoming.			
	after_start	normal	After Start	0		challenge	yes	no	0	Check compressor re-charges air bottle after start			
	taxi	normal	Taxi	0		challenge	yes	no	0	Use rudder bars for gentle turns			
	taxi	normal	Taxi	1		challenge	yes	no	0	Use burst of power to energize rudder when needed			
	taxi	normal	Taxi	2		challenge	yes	no	0	For tighter turns, use full rudder plus stick-mounted brake lever for differential braking			
	taxi	normal	Taxi	3		note	no	no	0	With rudders neutral, braking is equal to both main wheels.			
	taxi	normal	Taxi	4		caution	no	no	0	Take care not to reach excessive taxi speed; allow engine temperature to stabilize.			
	before_takeoff	normal	Engine Run-Up and Vital Actions	0		challenge	yes	no	0	Magnetos check			
	before_takeoff	normal	Engine Run-Up and Vital Actions	1		challenge	yes	no	0	Exercise RPM control to verify propeller governor operation			
	before_takeoff	normal	Engine Run-Up and Vital Actions	2		challenge	yes	no	0	Complete pre-takeoff vital actions using checklist			
	before_takeoff	normal	Engine Run-Up and Vital Actions	3		note	no	no	0	Max power (ceaseless engine function duration) is 5 minutes.			
	before_takeoff	normal	Engine Run-Up and Vital Actions	4		note	no	no	0	Throttle-engine lag (racing capacity) is 3 seconds max.			
	before_takeoff	normal	Engine Run-Up and Vital Actions	5		note	no	no	0	Max overspeed when operating throttle rapidly is 109 per cent.			
	before_takeoff	normal	Engine Run-Up and Vital Actions	6		note	no	no	0	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.			
	before_takeoff	normal	Engine Run-Up and Vital Actions	7		caution	no	no	0	Aerobatics forbidden with less than 4.5 gallons of fuel remaining.			
	takeoff	normal	Takeoff	0		challenge	yes	no	0	Apply full throttle			
	takeoff	normal	Takeoff	1		challenge	yes	no	0	Expect to push on the 'wrong' foot due to engine rotation direction			
	takeoff	normal	Takeoff	2		action	yes	no	0	Rotate	120 km/h (65 kt)		
	takeoff	normal	Takeoff	3		note	no	no	0	Take-off roll in ISA conditions is 590 ft at maximum weight.			
	after_takeoff	normal	After Takeoff	0		action	yes	no	0	Raise gear	BELOW 200 km/h (108 kt)		
	after_takeoff	normal	After Takeoff	1		challenge	yes	no	0	After selecting gear up, hold lever until 'three reds', then return lever to neutral			
	approach	normal	Circuit and Approach	0		action	yes	no	0	Lower gear	AT 200 km/h (108 kt)		
	approach	normal	Circuit and Approach	1		challenge	yes	no	0	After selecting gear down, hold lever until 'three greens', then return lever to neutral			
	approach	normal	Circuit and Approach	2		action	yes	no	0	Extend flaps	AT/OR BELOW 170 km/h (92 kt)		
	approach	normal	Circuit and Approach	3		action	yes	no	0	Fly approach	170 km/h (92 kt) slowing to 120 km/h (65 kt) at threshold		
	approach	normal	Circuit and Approach	4		note	no	no	0	Without flaps, forward view from rear seat is virtually nil; a curved approach is needed.			
	landing	normal	Landing	0		challenge	yes	no	0	Keep the canopy lock pin in place in the rail hole			
	landing	normal	Landing	1		challenge	yes	no	0	Lower nose after touchdown			
	landing	normal	Landing	2		note	no	no	0	High wing-loading means no tendency to float.			
	landing	normal	Landing	3		note	no	no	0	With practice, landing roll can be as short as 300 m (985 ft).			
	forced_landing	normal	Forced Landing	0		challenge	yes	no	0	Leave gear retracted for dead-stick landing			
	forced_landing	normal	Forced Landing	1		note	no	no	0	Standard drill is to leave gear retracted to flatten the descent profile.			
	forced_landing	normal	Forced Landing	2		note	no	no	0	Brakes remain usable with gear up.			
	forced_landing	normal	Forced Landing	3		note	no	no	0	With gear up, the undercarriage remains partially exposed to minimize damage in a wheels-up landing.			
	reference	normal	Reference	0		note	no	no	0	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.			
	reference	normal	Reference	1		note	no	no	0	Endurance in excess of 2 hours with 45 minutes reserve; maximum range 275 nm at slightly reduced cruise speed.			
	reference	normal	Reference	2		note	no	no	0	G limits: unlimited aerobatics certified at max takeoff weight 1,305 kg.			
	reference	normal	Reference	3		note	no	no	0	Engine: Ivchenko M-14P 9-cylinder radial, 360 hp.			
	reference	normal	Reference	4		note	no	no	0	Pneumatic system used for engine starting, flaps, gear, and brakes.			
	reference	normal	Reference	5		note	no	no	0	RPM gauge is calibrated in percent of maximum rather than RPM.			
	reference	normal	Reference	6		note	no	no	0	Artificial horizon is inverted in presentation: top half of ball is brown, bottom half is blue.			
	reference	normal	Reference	7		note	no	no	0	Rear cockpit has controls to deliberately fail certain systems in the front cockpit.			
	reference	normal	Reference	8		note	no	no	0	Gear lever is pneumatic and returns to central neutral position when not required.			
	reference	normal	Reference	9		note	no	no	0	Brakes are operated by a stick-mounted lever; pneumatic brake noise resembles a bus/lorry stopping.			
