107-II RFM Flashcards

1
Q

What type of engine is in the 107II?

A

CT58-104-2

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2
Q

What is two engine max continuous power

A

1250 SHP
No limit
NG - 100.3%
T5 - 660 deg C

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3
Q

What is one engine inoperative takeoff power?

A

1500 SHP
2-1/2 min
NG - 103.6%
T5 - 758 deg C

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4
Q

What is the single engine inoperative maximum continuous power

A

1400 SHP
30 min
NG - 100.3%
T5 - 696 deg C

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5
Q

What must be done if takeoff power is used in a cumulative excess of five minutes during any one emergency?

A

Engine must be inspected in accordance with the GE commercial engine maintenance manual

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6
Q

What is the NG overspeed limits range?

A

103.6% - 105.3% for 15 seconds

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7
Q

What is the NG overspeed limit?

A

105.3%

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8
Q

What is the maximum permitted speed for 2 1/2 minute single engine rating?

A

103.6%

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9
Q

What is the maximum permitted Nf speed for 15 seconds?

A

118.5%

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10
Q

What type of rotor blades for the 107II have?

A

Composite

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11
Q

What size fuel takes does the 107II have?

A

175 gal or 190 gal

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12
Q

What is Category “B” weight limits

A

landing and inground effect = 2000 lbs.

*Max weight maybe extended temp and altitude

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13
Q

What is the max takeoff weight for External Category “B” ?

A

2200 lbs. and maybe limited by the hover performance chart

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14
Q

When must an external load be jettisonable?

A

When any weights are above the takeoff, landing and in ground limits.

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15
Q

What is the Trans oil pressure?

A

20-85 psi

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16
Q

Where is the datum located in the 107II?

A

103.6” forward of the forward jacking point

17
Q

What are the start up limitations?

A

No more that 3 starts in any 30-min is prohibited.

*Unless in a emergency condition

18
Q

What is the max takeoff T5 temp?

A

696 deg C for 5 min.

*30 min during emergency

19
Q

What is the max continuous T5 temp?

A

660 deg C

20
Q

What is the max T5 temp for one engine at 2-1/2 min power?

A

758 deg C

21
Q

What is the oil pressure limits?

A

8-75 psi

22
Q

What is max contiguous power?

A

100% NR - 70% Torque

94% - 70%

23
Q

What is the Trans oil pressure?

A

20-85 psi

24
Q

Does the fuel boost pump need to be on for flight?

A

Yes

25
Q

What Pa must you descend to in the event of a boost pump failure?

A

4000’ Pa

26
Q

Usable fuel in a 175 gal tank?

A

2 gal

27
Q

The rotor break is prohibited when NR is below

A

40%

28
Q

What is the fuel pressure range?

A

190-995 psi

29
Q

What is the oil pressure limits?

A

8-75 psi

30
Q

is the 107II allowed to fly in known icing?

A

No

31
Q

are you permitted to crossfeed the tanks?

A

Emergency only and only up 400 lbs. remaining.

Ideal transfer is at 600 lbs.

32
Q

What is OAT is prohibited in visible moisture with engine inlet screens installed?

A

+2 deg C

33
Q

What temp must anti-ice and pitot heat be ON?

A

+4 deg C

34
Q

What is the limit for starting rotor in high winds?

A

gust in 16 kts.

35
Q

The rotor break is prohibited when NR is below

A

40%

36
Q

At what percent does the low fuel light come on at?

A

25% or 200 lbs. which gives you 20 min of fuel.

37
Q

what is the fuel burn for the 107II?

A

600 lbs. per hr., per engine.