Miscellaneous Flashcards

1
Q

ICING CONDITIONS

(In Visible Moisture and OAT Below +5C) What equipment must be ON, operative and utilized?

A
  1. Engine/propeller anti-ice systems
  2. Pitot heat/SAS heat
  3. Windshield heat
  4. Wing/empennage deice boots
  5. Continuous ignition system
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2
Q

The oxygen system includes a ______ oxygen supply cylinder.

A

49 cubic foot

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3
Q

Normal oxygen cylinder pressure is between ____ and ____ psi.

A

1600 and 1850

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4
Q

The NATO code for JP-8 is _____.

A

F-34

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5
Q

What is the minimum crew?

A

2 pilots

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6
Q

Starter limitations are:

A

30 sec on / 60 sec off (2 cycles)

30 sec on / 15 min off

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7
Q

Max continuous load for each generator is:

A

300 amps

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8
Q

Minimum oil pressure above 23,000 feet is:

A

50 psi

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9
Q

Max starting current from an external power source:

A

1,000 amps

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10
Q

Max fuel imbalance when fueling in gallons:

A

125 gal

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11
Q

Icing inhibitor fule additive:

A

MIL-L-27686E

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12
Q

Useable fuel quantity in gallons and liters:

A

648 gal

2453 liters

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13
Q

Max fuel imbalance for take-off, landing and normal flight:

A

200 pounds

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14
Q

Max shaft horsepower takeoff and continuous:

A

1,100 takeoff

1,000 continuous

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15
Q

Mixing oil types is allowed (T/F)

A

False

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16
Q

Engine/propeller system total oil quantity:

A

7.1 US quarts

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17
Q

Oil specification:

A

MIL-L-23699B (Type II)

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18
Q

Full reverse speed is limited to below _____ knots.

A

90

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19
Q

Takeoff with fuel transfer pump caution light(s) is:

A

prohibited

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20
Q

Autopilot/yaw damper use during fuel balancing is:

A

prohibited

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21
Q

G-limits Flaps Up

A

3.02 to -1.21

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22
Q

G-limits Flaps Down

A

2.00 to zero

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23
Q

During single engine taxi operations, nose wheel steering must be:

A

on

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24
Q

Main wheel tire limit

A

165 knots

25
Q

Nose wheel tire limit (with chines)

A

183 knots

26
Q

Minimum ambient temperature for engine ground start:

A

-40 C

27
Q

Minimum ambient temperature for engine operation:

A

-54 C

28
Q

Max ambient temperature allowed:

A

+37 C

29
Q

CAWI usage time is limited to:

A

5 minutes

30
Q

Max torque for CAWI use:

A

110%

31
Q

Max EGT for CAWI use:

A

650 C

32
Q

Max usable AWI fluid is:

A

14 US gallons

33
Q

Do not use CAWI if flued has been exposed to ________ within the preceding one hour.

A

-24 C

34
Q

Per the NFM, the maximum number of passenger seats permitted is_______.

A

18

35
Q

Max load aft of the cargo net:

A

600lbs

36
Q

Max AFT C.G. for the C-26:

A

277”

37
Q

Max operating pressure altitude:

A

25,000 feet

38
Q

Max normal cabin differential:

A

7.0 psi

39
Q

Cabin pressure safety valve is set to:

A

7.25 psi

40
Q

Aircrewmen shall fly once every ____ days.

A

60

41
Q

How many people is the life raft equipped for?

A

10

42
Q

Each generator produces _____ volts DC.

A

28.5

43
Q

Max ramp weight:

A

16,600

44
Q

Max take-off weight:

A

16,500

45
Q

Max landing weight:

A

15,675

46
Q

Max zero fuel weight:

A

14,500

47
Q

Max forward baggage compartment (nose) load:

A

800

48
Q

Max floor weight per square foot:

A

150 lb/sq ft

49
Q

Max aft baggage compartment load:

A

850

50
Q

Normal oil pressure below 23,000 feet:

A

70-120 psi

51
Q

Leave gear down at least ____ minutes to cool overheated brakes.

A

3 minutes

52
Q

Maximum psi of the aircrew oxygen bottle:

A

1850

53
Q

If a flashing wing overheat light does not extinguish within ____, the affected engine should be shut down.

A

3 minutes

54
Q

How many emergency exits are in the C-26?

A

five

55
Q

Normal hydraulic system operation pressure:

A

1,700 - 2,100 psi

56
Q

Battery output voltage:

A

24 volts

57
Q

Inverter output voltages:

A

115 and 25

58
Q

Airspeed Limits

1/4 Flaps
1/2 Flaps
Full Flaps

A

215 - 1/4 Flaps
180 - 1/2 Flaps
165 - Full Flaps