182 operating manual Flashcards

1
Q

minimum operating level of oil

A

9 quarts and replenish if below ten

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2
Q

If checking oil within 1 hour of engine operation the oil may appear _____

A

Low, as oil has not fully drained into the sump.

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3
Q

Start clearance call

A

Provide ATC with

Tug number, location (hanger 15), fuel on board (lbs), souls on board, intentions

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4
Q

Minimum temps for runup

A

OIL-T 75 degrees

CHT 200 degrees

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5
Q

to avoid shock cooling never go below___ degrees in cooling

A

60 degrees per min

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6
Q

stall recovery

A

A. P-Push the nose forward, if wing drops use opposite rudder

B. P-power. Apply full power simultaneously with lowering the nose

C. after recovering from the stall, raise any flaps in steps and establish a climb to a
safe altitude.

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7
Q

spin recovery

A

P – Power – bring throttle to idle.
A – Ailerons – centralize the control column. Raise flaps if required;
R – Rudder – apply full rudder opposite to the direction of rotation;
E – Elevator – ease the yoke forward to break the stall; and

once rotation stops, centralize the rudders, level the wings, ease out of the ensuing dive, and establish a climb to a safe altitude.

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8
Q

spiral dive recovery

A

P – Power – reduce power to idle;
R – Roll – roll to a wings level attitude with full aileron deflection;
P – Pull – pull the nose up to ease out of the ensuing dive; and

after recovery from the spiral dive, apply power as required to establish a climb to a safe altitude.

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9
Q

unusual attitudes- Nose high

A

P – Power – apply full power to help prevent the aircraft from stalling;
R – Roll – roll the aircraft toward the nearest horizon and maintain slight positive “G,” but avoid excessive back pressure on the yoke because of the danger of stalling. Increasing the angle of bank toward the nearest horizon provides the shortest route towards the horizon by reducing the lift vector holding the nose above the horizon. At a 90 degree angle of bank, there is no lift holding the nose above the horizon.
R – Roll – roll out to wings level as the nose reaches the horizon and airspeed is increasing to a safe flying speed. Allow the nose to pass through and below the horizon as necessary for gaining a safe flying speed.

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10
Q

unusual attitudes- nose low

A

The nose low unusual attitude recovery procedure is the same as for a spiral dive recovery.

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11
Q

traffic pattern entry/ engine management

A

a. slowing to approximately 125 MPH can be accomplished with a power setting of 2400 RPM and 20” MAP;
b. if desired, a slower airspeed of approximately 115 MPH can be achieved with power setting of 2400 RPM and 18” MAP. At this airspeed, it is recommended to select flaps to 10 degrees to prevent an excessive nose-up attitude in the circuit; and
c. if desired, higher throttle settings / higher airspeeds may be used, but will require careful circuit planning to permit deceleration to Vfe without creating an unusually high / fast final approach.

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12
Q

approach speed 0 degree flaps

A

80-90 MPH IAS

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13
Q

approach speed 20 degrees flaps

A

75-85 MPH IAS

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14
Q

Approach speed 35 degrees flaps

A

70-80 MPH IAS

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15
Q

Short field landing

A

35 degrees flaps and IAS of 70 MPH

normal shortfield approach and landing

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16
Q

glider release procedure/ level on tow

A

a. coming up to release alt. reduce MAP to around 16” while maintaining 70mph (level off)
b. Close cowl flaps
c. await glider release. visually confirm release with falling rope and climbing right turn

17
Q

Decent after release

A

Primary Descent Profile:
a. reduce throttle to 21-23” MAP;

b. retract flaps to 0°;
c. ensure the cowl flaps are closed;
d. reduce propeller speed to 2300 RPM for noise abatement;
e. increase IAS to approximately 130 MPH;
f. initial cooling rate should be approximately 40° to 60° /minute;
g. monitor the cooling rate and maintain at less than 60° /minute;
h. as the cooling rate decreases to about 40° /minute, reduce power to 18” MAP;
i. cooling rate will increase, and then begin to decrease;
j. when back down to approximately 40° /minute, reduce power by 2” of MAP;

k. continue repeating this
cycle until at about 13” MAP;

l. reduce IAS to below 110 MPH and lower 10° of flap;
m. extend up to full flap below 90 MPH; and
n. complete a circuit and landing IAW local procedures.