Type Exam #1

Question 1

What are the max internal and external gross weight limits?

Answer 1

3200lbs

3350lbs

Question 2

What is the VNE between 85% and 100% torque power range?

Answer 2

92 MPH

Question 3

What is the VNE when gross weight is 3000lbs?

Answer 3

150MPH

Question 4

What is the VNE when gross weight is above 3000lbs

Answer 4

140MPH

Question 5

What is max operating altitude for gross weights of 3000lbs and below?

Answer 5

20 000 feet pressure altitude

Question 6

Min and max rotor RPM (Nr) with power off?

Answer 6

90% and 107%

Question 7

Min rotor RPM for gross weights above 3000lbs is ________ and can droop down to ________ for max of _______ seconds

Answer 7

97%
95%
5 seconds

Question 8

Which engine is in Bell 206B2?

Answer 8

Allison 250-C20

Question 9

Max Power Turbine N2 RPM is ________ and min is _________ when gross weights above 3000lbs?

Answer 9

100%

97%

Question 10

N2 transient over speed limit is _____ for max of ______ seconds

Answer 10

105%

15 seconds

Question 11

The max Gas producer (N1) RPM is ________ and transient limit is _______ for max of _________ seconds?

Answer 11

104%
105%
15 seconds

Question 12

Max allowable engine oil temp?

Answer 12

107 C

Question 13

Max takeoff torque is _______ for a max of _______ minutes?

Answer 13

100%

5 minutes

Question 14

Max continuous torque is _________ with max TOT of _________?

Answer 14

85%

737 C

Question 15

Max TOT limit for take off?

Answer 15

793 C for 5 minutes

Question 16

What are transient TOT limits?

Answer 16

793 C to 843 C for 6 seconds

Question 17

What are Max starting and shut down TOT limits?

Answer 17

793 C to 927 C for 10 seconds

Question 18

Anti icing must be on for flight in visible moisture when temp is below _______?

Answer 18

4.4 C

Question 19

Max transmission oil pressure is ________ and max transmission oil temp is ________?

Answer 19

70 PSI

110 C

Question 20

Above 8000 feet what are the min and max N2 limits?

Answer 20

97%

100%

Question 21

Min front seat weight?

Answer 21

150lbs

Question 22

The C of G longitudinal limits from station are?

Answer 22

106 inches to 114.2 inches

Question 23

What are the later C of G limits?

Answer 23

3 inches left

4 inches right

Question 24

When staring when should fuel be introduced N1?

Answer 24

15%

Question 25

If main rotor is not turning by ______ N1 start should be aborted.

Answer 25

25%

Question 26

On start up the starter should be released at _______ N1?

Answer 26

58%

Question 27

When should the generator be turned on? (N1)

Answer 27

100%

Question 28

If engine has been shut down for more than 15 min engine must stabilize at ground idle speed for ________ before increasing power?

Answer 28

1 minute

Question 29

Before takeoff the generator load should be below ______?

Answer 29

70%

Question 30

On shutdown how long should engine stabilize at idle speed before the throttle is closed?

Answer 30

2 minutes

Question 31

When both fuel pumps become inoperative the unusable fuel becomes________ gallons?

Answer 31

10 gallons

Question 32

If one or both boost pumps become inoperative descend below?

Answer 32

6000 feet pressure altitude

Question 33

What is the desired airspeed in autorotation?

Answer 33

58 to 69 MPH

Question 34

During hydraulic system failure the airspeed should be reduced to ______ ?

Answer 34

70 to 80 MPH

Question 35

Area B in critical wind azimuth chart is from ______ to _______ degrees?

Answer 35

50 to 210 degrees

Question 36

C of G will ______ as fuel is consumed?

Answer 36

Move fwd

Question 37

Baggage compartment has load limit of ______ lbs with max of _______ lbs per square foot?

Answer 37

250 lbs and 86 lbs

Question 38

With single bladder fuel cell total capacity is ______ US Gallons and the useable fuel capacity is ______ US gallons?

Answer 38

77.06 and 76 US gallons

Question 39

Engine oil capacity?

Answer 39

5.5 US Quarts

Question 40

Max tie down load applied to blade tips shall not exceed_______ ?

Answer 40

100 lbs

Question 41

With Range extender fuel system installed the min cockpit weight becomes ________ lbs ?

Answer 41

200 lbs

Question 42

With range extender fuel system installed the baggage compartment is restricted to ________ lbs when Aircraft is loaded with 3 rear pax?

Answer 42

110 lbs

Question 43

What is max capacity with range extender full (US Gallons)

Answer 43

96.7 US Gallons

Question 44

When external cargo hook is installed what is the VNE when flying a sling load above 3000 lbs gross weight?

Answer 44

91 MPH

Question 45

External cargo hook model 206-706-335 has max load of ______ lbs?

Answer 45

1500 lbs

Question 46

With particle separator engine air induction system the deflector baffled shall be removed at _____ f OAT and above?

Answer 46

80 degrees f

Question 47

When engine re-ignition system is installed it should not be activated above _______ ft?

Answer 47

12 000 feet

Question 48

What is the VNE with one or both aft cabin doors of up 3000 feet?

Answer 48

100 MPH

Question 49

What is the VNE with one or both forward doors off all or any combination of fwd and aft doors off?

Answer 49

80 MPH

Question 50

With fwd or aft doors removed the VNE decreases _______

Answer 50

1 MPH per 1000 feet above 3000 feet