DASH ONE: SECTION 2 (Normal procedures) Flashcards

You should be able to describe all the info from the deck

1
Q

CAUTION

What is important to remember when opening the canopy?

A

CAUTION

The canopy should always be supported by hand until fully opened.

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2
Q

What are we checking for during an EXTERIOR INSPECTION?

A

Cracks, distortions, loose or missing items, fluid leakage and general cleanliness.

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3
Q

NOTE

What is an EXTERIOR INSPECTION?

A

NOTE
The EXTERIOR INSPECTION in done to check the airplane for general condition. If anything abnormal is observed, notify the crew chief.

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4
Q

NOTE

If no technical assistance the aircraft fire extinguisher __ __ __ __ ___ __ __ _ __ _____.

A

NOTE

If no technical assistance the aircraft fire extinguisher may be the only means to fight a fire hazard.

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5
Q

NOTE

Correct fuel indication can only be obtained __ ___ _ _ __ ___.

A

NOTE

Correct fuel indication can only be obtained when aircraft is in level position.

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6
Q

NOTE

What can we do to stop draining the fuel from the vent lines?

A

NOTE
To stop draining of fuel from the vent lines, ground operation should be performed on one fuel tank.
For eksempel LEFT ON eller RIGHT ON

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7
Q

NOTE

If oil temp. is above 50°C - what can we omit?

A

NOTE

If oil temp. is above 50°C omit step 12-14 in starting engine checklist.

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8
Q

CAUTION
Explain the starter system, how long you can engage the starter button in one start attempt, how long is the cool down between and how many times you can do it before you need to allow the starter to cool for 30 minutes.

A

CAUTION
Do not engage starter for more than 10 seconds in one start attempt. Allow 20 seconds for starter cool-down between each attempt. this start cycle can be repeated up to six times. If however repeated six times, allow starter to cool for 30 minutes.

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9
Q

CAUTION

What will happen if the RH magneto switch is turned on before the engine fires?

A

CAUTION
If the RH magneto switch is turned on before the engine fires, the engine will probably backfire thus damaging the starter.

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10
Q

CAUTION

If minimum oil pressure (25 psi) is not indicated within “…” after engine start, stop engine.

A

CAUTION

If minimum oil pressure (25 psi) is not indicated within 30 seconds after engine start, stop engine.

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11
Q

NOTE
After “Engine Start” the GEN caution light may illuminate due to low system voltage, when can this condition be accepted only?

A

NOTE

This condition can be accepted on GND only. Take-off must not be initiated with GEN caution light illuminated.

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12
Q

NOTE

After “Engine Start” the engine RPM should be what? What should you avoid during ground operation and after start-up?

A

NOTE
After “Engine Start” the engine RPM should be 1200RPM whenever possible. Avoid prolonged engine ground operation at “idle” RPM. Avoid rapid engine speed changes after start-up, and use only the power settings required to taxi.

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13
Q

CAUTION

When parked avoid less than 1200 RPM since this may what?

A

CAUTION
When parked avoid less than 1200 RPM since this may damage the engine and increase the settling of lead in cylinders and on sparkplugs.

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14
Q

CAUTION

What RPM should you not exceed on ground except during take-off?

A

CAUTION

Do not exceed 2500 RPM on ground except during take-off.

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15
Q

CAUTION

Pilots should avoid run-up in areas with loose articles (gravel, stone etc.), why?

A

CAUTION
“because the suction from the propeller may lift these articles and thereby cause damage to the propeller and other sections of the aircraft body.”

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16
Q

NOTE

If night flying is planned, what should you check and what should you make sure is available?

A

NOTE

If night flying is planned, check operation of all lights, internal/external, and make sure a flash light is available.

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17
Q

TAXIING

Never attempt taxiing in wind velocities of more than?

A

TAXIING

Never attempt taxiing in wind velocities of more than 50 kts.

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18
Q

CAUTION

Taxiing in slush may cause what? What can you do to prevent it?

A

CAUTION
Taxiing in slush may cause the static ports to get blocked by ice due to splash from the main wheels. Therefore taxi speed should be as low as possible.

19
Q

NOTE
If requirements in checks 1-4 in engine run-up are not met (RPM stabilized within the limits checks) what should you then do?

A

NOTE
If requirements in checks 1-4 are not met, warm up engine until ENG OIL TEMP is in the normal operating range, and then perform a new check.

20
Q

NOTE

Caution must be exercised to return the Mixture control Leaver to Full Rich before what?

A

NOTE
Caution must be exercised to return the Mixture control Leaver to Full Rich before the RPM can drop to a point where the Engine Cuts Out.

21
Q

NOTE (During mixture check)
An RPM increase of 50 RPM or more indicates an excessively Rich Idle Mixture. An Immediate decrease in RPM , if not preceded by an increase indicates what?

A

NOTE

An Immediate decrease in RPM, if not preceded by an increase, indicates the Idle Mixture is too Lean.

22
Q

NOTE

If “Engine Run-Up” shows magneto drop out of limit and/or uneven engine run, perform peak lean. Explain peak lean.

A

NOTE
If “Engine Run-Up” shows magneto drop out of limit and/or uneven engine run, then, with both magnetos “ON”, set RPM to 2500 RPM, lean to peak EGT, and run the engine for 30-40 seconds at peak EGT, then reduce to 1200 RPM and select mixture rich. Perform a new engine run-up check. If magneto drop is still out of limits, ground abort aircraft.

23
Q

CAUTION
Avoid rapid opening and/or closing of the throttle, as this may what? Full range throttle movements should be performed over a minimum duration of how long?

A

CAUTION Avoid rapid opening and/or closing of the throttle, as this may detune the crankshaft counterweights with subsequent engine damage. Full range throttle movements should be performed over a minimum duration of 2 seconds.

24
Q

NOTE

After nose wheel lift-off, the nose wheel strut will “…”, and directional control is maintained by “…”

A

NOTE
After nose wheel lift-off, the nose wheel strut will automatically lock in center position, and directional control is maintained by rudder only.

25
Q

NOTE

“…” of the aircraft during take-off, will increase ground roll distance.

A

NOTE

Over-rotation of the aircraft during take-off, will increase ground roll distance.

26
Q

NOTE
When take-off is performed with engine oil temperature below normal operating range (green area) a higher than normal engine RPM may be expected. What should you do under these circumstances?

A

NOTE
Under these circumstances the propeller lever should be retarded to 2700 RPM in order not to exceed the maximum engine RPM limit.

27
Q

NOTE
Before “Engine Shut Down” engine RPM should be set at “…” until oil temperature has stabilized.
Unless inconvenient due to environmental conditions, RPM should be increased to “…” before “Mixture - CUT OFF for a period of “…”.

A

NOTE
Before “Engine Shut Down” engine RPM should be set at 1200 RPM until oil temperature has stabilized.
Unless inconvenient due to environmental conditions, RPM should be increased to 1800 RPM before “Mixture - CUT OFF for a period of 15-20 sec.

28
Q

NOTE

Where should the shoulder harness be placed when leaving the aircraft?

A

NOTE

When leaving the cockpit make sure that the shoulder harness is inside before closing the canopy.

29
Q

CAUTION

When leaving the aircraft, what should we do with the canopy and why?

A

CAUTION
Do not leave the aircraft with an open canopy. Strong winds can damage hinges/dampers. Furthermore the canopy could in some cases converge sun rays making it a fire hazard.

30
Q

NOTE

Minimum RPM for take-off with full power is what?

A

NOTE

Minimum RPM for take-off with full power is 2670.

31
Q

CAUTION

Too rapid movement of the throttle may cause ___ __ ___.

A

CAUTION

Too rapid movement of the throttle may cause engine over speed.

32
Q

NOTE
For a no-flap landing increase ___ and ___ speeds by _ kts.
If the aircraft gross weight is above ____ kg, increase ___ and ___ speeds by _ kts.
When winds are gusty, add _____ the gust factor ____ airspeed.

A

NOTE
For a no-flap landing increase base and final speeds by 5 kts.
If the aircraft gross weight is above 1050 kg, increase base and final speeds by 5 kts.
When winds are gusty, add one-half the gust factor final airspeed.

33
Q

MAXIMUM PERFORMANCE TAKE-OFF

Discribe a maximum performance take-off.

A

MAXIMUM PERFORMANCE TAKE-OFF
For maximum performance take-off use 10 degrees flaps. When lined up on the runway apply full throttle and when RPM passes through 2500 RPM release the brakes. For take-off run use the same procedure as for normal take–off. ROTATION and LIFT-OFF SPEED should be 5 kts lower than normal.

34
Q

CROSSWIND TAKE-OFF

Discribe a crosswind take-off.

A

CROSSWIND TAKE-OFF
For crosswind take-off it is recommended not to use flaps and to keep the nose wheel on ground until lift-off speed is obtained.

35
Q

WARNING

If ALT STATIC AIR is selected, ___ __ __ ___ ___ _ __ ___.

A

WARNING

If ALT STATIC AIR is selected, increase base and final speeds by 10 kts.

36
Q

CAUTION

When using a high power setting, what is important to remember to do before selecting high RPM?

A

CAUTION

If using a high power setting, reduce power before selecting high RPM.

37
Q

NOTE
TO INCREASE POWER - first, ____ ____, then ____ ___ ___.
TO DECREASE POWER - first ____ ____, and then ___ ___.

A

NOTE
TO INCREASE POWER - first, enrich mixture, then follow with throttle.
TO DECREASE POWER - first, reduce throttle, and then adjust mixture.

38
Q

NOTE

When should the strobe lights be switched off during flight?

A

NOTE

Strobe lights should be switched off if flashes interferes with aircraft operation (IMC).

39
Q

WARNING

Correcting a fuel imbalance by skidding the aircraft under IMC __ ___ ___ _____.

A

WARNING

Correcting a fuel imbalance by skidding the aircraft under IMC may cause spatial disorientation.

40
Q

NOTE

With passengers in the front seat what should you be aware of?

A

NOTE
With passengers in the front seat, exervise extreme caution if retarding mixture beyond the detent, as the passengers may cut off of the fuel unintentionally.

41
Q

NOTE
To correct a fuel imbalance, place the fuel selector in position __ __ and yaw (skid) the aircraft to the side with __ fuel state, using ____ ball width. This skid will transfer fuel from one tank through the fuel selector to the other tank.

A

NOTE
To correct a fuel imbalance, place the fuel selector in position BOTH ON and yaw (skid) the aircraft to the side with low fuel state, using ½-1 ball width. This skid will transfer fuel from one tank through the fuel selector to the other tank.

42
Q

NOTE

Flying with the fuel selector in position BOTH ON, may cause what? and what can we do to stop the situation?

A

NOTE
Flying with full tanks and the fuel selector in position BOTH ON may cause siphoning of fuel from either tank. To correct the situation, place the fuel selector in position LEFT or RIGHT ON and the siphoning will stop within 10-15 sec.

43
Q

NOTE

When airborne the auxiliary fuel pump should be ON during the following conditions?

A

NOTE
When airborne the auxiliary fuel pump should be ON during the following conditions:
-When flying below 500 ft AGL.
-During any airborne utilization of the fuel selector, until the operator is assured that there will be no interruption of the fuel flow ( 5 seconds)
-Any time the fuel flow is fluctuating or the engines is affected by the fluctuation,

44
Q

LANDING
Standard base speed?
Standard final speed?

A

80 kts

75 kts