V Speeds Flashcards
VNE (44)
202 red line
VNO (44)
169
VA (44)
135 kts @ 3800
112 kts at 2700
VFE (44)
111
VLE (44)
140 (gear extended speed)
VLO
111 extending gear
140 retracting gear
One engine Vy
88 blue line
VMC
56
Yellow arc
169-202 caution
Green arc
57-169 normal
White arc
55-111 flaps
VSSE
82 intentional one engine speed
VMCA demonstration
Landing gear up
Flaps up
Airspeed 82 1850 rpm
Mixture rich
Prop high rpm
Inoperative engine idle
OE full throttle
Airspeed reduce 1 kt per second until horn
Vr (44)
74
Engine operating limits 44
180 hp
Max rpm 2700
Max manifold pressure full throttle
Max cylinder head temp 500
Max oil temp 245
Max oil press 115
Min oil press 25
Normal fuel press .5-8
110 gal 108 usable
Hartzell prop 72-74 in
Weights (44)
Ramp 3816
TO 3800
Baggage 200
Engine out less than 75 or gear down checklist 44
Throttles ……………………………………………………….IMMEDIATELY CLOSE Brakes (or land and brake)……………………………………………AS REQUIRED Stop straight ahead
If insufficient runway remains for a complete stop:
Mixtures……………………………………………………………………..IDLE CUTOFF Fuel Selectors ……………………………………………………………………………..OFF Magneto Switches………………………………………………………………………..OFF Battery Master Switch ………………………………………………………………….OFF Maintain directional control, maneuvering to avoid obstacles if necessary.
Engine out during TO above 75
Directional Control …………………………………………………………..MAINTAIN Throttles ……………………………………………………….IMMEDIATELY CLOSE Land straight ahead
Brakes ……………………………………………………………………….AS REQUIRED
Engine out during TO and you commit to taking off
Mixture controls ……………………………………………………..FULL FORWARD Propeller controls…………………………………………………….FULL FORWARD Throttle controls ……………………………………………………..FULL FORWARD Flaps…………………………………………………………………………………..FULL UP Landing Gear Selector……………………………………………………….CHECK UP Inoperative Engine………………………………………….IDENTIFY and VERIFY Throttle (Inop. Engine)…………………………………………………………….CLOSE Propeller (Inop. Engine)………………………………………………………FEATHER Mixture (Inop. Engine)………………………………………………..IDLE CUT-OFF Establish Bank …………………………….2° to 3° INTO OPERATIVE ENGINE Climb Speed …………………………………………………………………………88 KIAS Trim ………………………………………………………..ADJUST TO 2° to 3° BANK
TOWARD OPERATIVE ENGINE WITH APPROXIMATELY 1/2 BALL SLIP INDICATED ON THE TURN AND BANK INDICATOR Cowl Flap (Inop. Engine)…………………………………………………………CLOSE Alternator Switch (Inop. Engine) …………………………………………………..OFF Magneto Switches (Inop. Engine) ………………………………………………….OFF Electric Fuel Pump (Inop. Engine) …………………………………………………OFF Fuel Selector (Inop. Engine)………………………………………………………….OFF
Land as soon as practical at the nearest suitable airport.
ENGINE FAILURE DURING CLIMB
Airspeed…………………………………………………………….MAINTAIN 88 KIAS Directional Control …………………………………………………………..MAINTAIN Power………………………………………………………………MAX. CONTINUOUS Inoperative Engine …………………………………………IDENTIFY and VERIFY Inoperative Engine …………………………………………………….Complete Engine
Securing Procedure Trim………………………………………………………..ADJUST TO 2° to 3° BANK TOWARD OPERATIVE ENGINE WITH APPROXIMATELY 1/2 BALL SLIP INDICATED ON THE TURN AND BANK INDICATOR Cowl Flap (Operative Engine)………………………………………AS REQUIRED
Land as soon as practical at the nearest suitable airport.
ENGINE FAILURE DURING FLIGHT (SPEED ABOVE VMCA)
Inoperative Engine……………………………………………………………..IDENTIFY Operative Engine……………………………..ADJUST POWER AS REQUIRED Airspeed ……………………………………………………ATTAIN AND MAINTAIN
Before securing inop. engine:
Electric Fuel Pump………………………………………………………………………..ON Fuel Quantity……………………………………………………………………….. CHECK Oil Pressure and Temperature ………………………………………………….CHECK Magneto Switches ………………………………………………………………….CHECK Air Start…………………………………………………………………………….ATTEMPT
If engine does not start, complete Engine Securing Procedure.
Power (Operative Engine) ……………………………………………AS REQUIRED Fuel Quantity (Operative Engine Tank) …………………………….SUFFICIENT Electric Fuel Pump (Operative Engine)………………………….AS REQUIRED Cowl Flap (Operative Engine)………………………………………AS REQUIRED Trim ………………………………………………………..ADJUST TO 2° to 3° BANK
TOWARD OPERATIVE ENGINE WITH APPROXIMATELY 1/2 BALL SLIP INDICATED ON THE TURN AND BANK INDICATOR Electrical Load ……………………………….DECREASE TO MIN. REQUIRED
Land as soon as practical at the nearest suitable airport.
ONE ENGINE INOPERATIVE LANDING
Inoperative Engine………………………..ENGINE SECURING PROCEDURE COMPLETE Seat Belts/Harnesses……………………………………………………………..SECURE Fuel Selector (Operative Engine)…………………………………………………….ON Mixture (Operative Engine) ………………………………………………FULL RICH Propeller Control (Operative Engine)…………………………FULL FORWARD Electric Fuel Pump (Operative Engine) ……………………………………………ON Cowl Flap (Operative Engine)………………………………………AS REQUIRED
Altitude & Airspeed…………………………………………………MAKE NORMAL APPROACH
When Landing is Assured:
Landing Gear …………………………………………………………………………DOWN Wing Flaps …………………………………………………………………25° (2nd Notch) Final Approach Speed …………………………………………………………..90 KIAS Power ………………………………………………………….RETARD SLOWLY AND
FLARE AIRPLANE Trim ………………………………………………………….AS POWER IS REDUCED (AIRPLANE WILL YAW IN DIRECTION OF OPERATIVE ENGINE)
ONE ENGINE INOPERATIVE GO-AROUND (Should be avoided if at all possible)
Mixture ……………………………………………………………………………FORWARD Propeller…………………………………………………………………………..FORWARD Throttle……………………..SMOOTHLY ADVANCE TO TAKEOFF POWER Flaps………………………………………………………………….RETRACT SLOWLY Landing Gear……….RETRACT (AFTER POSITIVE CLIMB ACHIEVED) Airspeed……………………………………………………………………………….88 KIAS Trim ………………………………………………………..ADJUST TO 2° to 3° BANK
TOWARD OPERATIVE ENGINE WITH APPROXIMATELY 1/2 BALL SLIP INDICATED ON THE TURN AND BANK INDICATOR Cowl Flap (Operating Engine)………………………………………AS REQUIRED
UNFEATHERING PROCEDURE/ UNFEATHERING ACCU- MULATOR FUNCTIONING
With the propeller unfeathering system installed, the propeller will usually windmill automatically when the propeller control is moved forward.
Fuel Selector (Inoperative Engine) ………………………………………………….ON Magneto Switches (Inoperative Engine) …………………………………………..ON Electric Fuel Pump (Inoperative Engine)………………………………………….ON Mixture ………………………………………………………………………….FULL RICH Throttle ………………………………………………………………………..Open 1/4 inch
Prop Control ………………………………………………………….FULL FORWARD Throttle …………………………………………………………………Reduce power until engine is warm Alternator …………………………………………………………………………………….ON
