Kap 1

Question 1

In case of total oil pressure loss

Answer 1

In case of total oil pressure loss the propeller blades move into coarse pitch (low rpm), thus preventing engine over speed.

Question 2

Due to the constant speed propeller,

Answer 2

Due to the constant speed propeller, opening of the throttle will increase the manifold pressure, not necessarily the RPM.

Question 3

Straight and level coordinated flight

Answer 3

Straight and level coordinated flight is required for the most accurate indication of the fuel quantity, but with partly filled tanks each fuel indicator may i.a.w. the technical specifications show as much as 3,5 US Gall more than the actual quantity, -and with completely empty tanks indicators may show as much as 2 Gall in each tank.

Question 4

To operate the Standby Attitude Indicator,

Answer 4

To operate the Standby Attitude Indicator, the VHF 2 COM radio and the map lights the EPU switch must be switched in ON position. Leaving the EPU in ON after aircraft shutdown could result in EPU battery discharge or damage.

Question 5

The EPU switch shall

Answer 5

The EPU switch shall be in OFF position whenever external power is connected to the aircraft,

Question 6

BAT switch shall be in

Answer 6

BAT switch shall be in OFF position when external power is used, otherwise the external power is shut off.

Question 7

When the aircraft has been exposted to moisture and/or icing conditions

Answer 7

When the aircraft has been exposted to moisture and/or icing conditions (especially on the ground), the possibility of obstructed static ports should be considered. Partial obstructions will result in the rate of climb indication being sluggish during a climb or descent. Verification of suspected obstruction is possible by switching to the ALT STATIC AIR system and noting a sudden sustained change in the rate of climb. This may be accompanied by an increase in indicated airspeed of 5-10 kts and altitude changes beyond normal calibration differences.

Question 8

When the aircraft has been exposted to moisture and/or icing conditions (especially on the ground), the possibility of obstructed static ports should be considered. Partial obstructions will result in the rate of climb indication being sluggish during a climb or descent. Verification of suspected obstruction is possible by switching to the __________ system and noting a sudden sustained change in the rate of climb. This may be accompanied by an increase in indicated airspeed of ______ and altitude changes beyond normal calibration differences.

Answer 8

When the aircraft has been exposted to moisture and/or icing conditions (especially on the ground), the possibility of obstructed static ports should be considered. Partial obstructions will result in the rate of climb indication being sluggish during a climb or descent. Verification of suspected obstruction is possible by switching to the ALT STATIC AIR system and noting a sudden sustained change in the rate of climb. This may be accompanied by an increase in indicated airspeed of 5-10 kts and altitude changes beyond normal calibration differences.

Question 9

If the altimeter´s internal vibrator is inoperative,

Answer 9

If the altimeter´s internal vibrator is inoperative, the pause-and-accelerate effect may be exaggerated. The pilot should be especially watchful for this behavior, when the minimum approach altitued lies within the “8” to “2”, sector of the sector of the scale, e.g., 800-1200 feet, 1800-2200 feet, etc.

Question 9

If the altimeter´s internal vibrator is inoperative,

Answer 9

If the altimeter´s internal vibrator is inoperative, the pause-and-accelerate effect may be exaggerated. The pilot should be especially watchful for this behavior, when the minimum approach altitued lies within the “8” to “2”, sector of the sector of the scale, e.g., 800-1200 feet, 1800-2200 feet, etc.

Question 10

The CO-indicater

Answer 10

The CO-indicator is located above the radio panel. Presence of CO will gradually turn the indicator black.

Question 11

If no technical assistance the aircraft fire extinguisher

Answer 11

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

Question 12

Do not engage starter for more than _______ in one start attempt.
Allow _________ for starter cool-down between each attempt.
This cycle can be repeated up to ________.
If however repeated ________, allow starter to cool for _________.

Answer 12

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

Question 13

If the RH magneto swich is turned on before

Answer 13

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

Question 14

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

Answer 14

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

Question 15

If minimum oil pressure (_____) is not indicated within _________ after engine start, stop engine.

Answer 15

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

Question 16

After “Engine Start” the ____ caution light may illuminate due to low system voltage. This condition can be accepted on ____ only. Take-off must not be initiated with _____ caution light illuminated.

Answer 16

After “Engine Start” the GEN caution light may illuminate due to low system voltage. This condition can be accepted on GND only. Take-off must not be initiated with GEN caution light illuminated.

Question 17

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

Answer 17

After “Engine Start” the engine RPM should be 1200 RPM 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.

Question 18

When parked avoid less than ________ since this may damage the engine and increase the settling of ____ in the cylinders and on the __________.

Answer 18

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

Question 19

When parked avoid less than 1200 RPM

Answer 19

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

Question 20

Do not exceed ____________ except during take-off.

Answer 20

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

Question 21

Pilots should avoid ______ in areas with ________ (gravel, stone etc.), because the suction from the propeller may lift these articles and thereby cause __________ to the __________ and other sections of the aircraft body.

Answer 21

Pilots should avoid run-up in areas with loose articles (gravel, stone etc.), because the suction from the propeller may lift these articles and thereby cause damage to the propeller and other sections of the aircraft body.

Question 22

Taxiing in slush

Answer 22

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

Question 23

When making sharp turns,

Answer 23

When making sharp turns, centrifugal forces may cause fuel overflow, from the outboard tank. This is especially the case when the fuel selector is in position BOTH ON. To stop siphoning of fuel from either tank, select left or right tank ON.

Question 24

When making sharp turns, ___________ may cause ___________, from the outboard tank. This is especially the case when the fuel selector is in position ___________. To stop siphoning of fuel from either tank, select __________.

Answer 24

When making sharp turns, centrifugal forces may cause fuel overflow, from the outboard tank. This is especially the case when the fuel selector is in position BOTH ON. To stop siphoning of fuel from either tank, select left or right tank ON.

Question 25

If requirements in checks _____ are not met, warm up engine until __________ is in the ________, and then perform a _______.

Answer 25

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.

Question 26

Caution must be ______ to return the Mixture control Leaver to _______ before the RPM can drop to a point where the Engine _______.

Answer 26

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.

Question 27

An RPM increase of 50 RPM or more indicates an excessively Rich Idle Mixture.

Answer 27

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 the Idle Maxture is too Lean.

Question 28

________________ coordinated flight is required for the most accurate indication of the fuel quantity, but with partly filled tanks each fuel indicator may i.a.w. the technical specifications show as much as _________ more than the actual quantity, -and with completely empty tanks indicators may show as much as _______ in each tank.

Answer 28

Straight and level coordinated flight is required for the most accurate indication of the fuel quantity, but with partly filled tanks each fuel indicator may i.a.w. the technical specifications show as much as 3,5 US Gall more than the actual quantity, -and with completely empty tanks indicators may show as much as 2 Gall in each tank.

Question 29

To operate the ________ , __________ and _____ the EPU switch must be switched in ___ position.
Leaving the EPU in ON after aircraft shutdown could result in EPU battery ________ or ___________.

Answer 29

To operate the Standby Attitude Indicator, the VHF 2 COM radio and the map lights the EPU switch must be switched in ON position. Leaving the EPU in ON after aircraft shutdown could result in EPU battery discharge or damage.