LIMITATIONS Flashcards

1
Q

Where is the Datum located in Short Nose?

A

Approx 6” forward of the nose cone fairing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Where is the Datum located in Long Nose?

A

Approx 21” aft of the tip of the nose cone fairing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Where is the CG Range T/O and LDG (all series @ all weight on wipline floats)

A

Forward 207.74 in (25% MAC)
Aft 213.20 in (32% MAC)
Ref datum 60” forward of front fuselage bunk head

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Mass Limitations for 100/200

A

M. T/O- 11,600 lbs
M. LDG- 11,600 lbs
M. 0 Fuel- 11,400 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Mass limitations for 300

A

M. T/O- 12,500 lbs
M. LDG- 12,500 lbs
M. 0 Fuel- 12,300 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

VMO for 100/200

A

158 up to 10,000ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Vp/Va/Vb for 100/200

A

129

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Vmc flaps 10 for 100/200

A

67

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Vmc flaps 20 for 100/200

A

67

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

VMO for 300

A

158 decrease by 1 every 1000ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Vp/Va/Vb for 300

A

135

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Vmc flaps 10 for 300

A

70

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Vmc flaps 20 for 300

A

67

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

VFE flaps 0-20 for 100/200

A

100

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

VFE flaps 20-37.5 for 100/200

A

85

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

VFE flaps 0-10 for 300

A

102

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

VFE flaps 10-37.5 for 300

A

95

17
Q

Vx

A

82

18
Q

Vy

A

90

19
Q

Vyse flaps 10

A

86

20
Q

Vno flaps 0

A

120

21
Q

minimum manoeuvring speed flaps 0

A

100

22
Q

minimum manoeuvring speed flaps 10

A

90

23
Q

minimum manoeuvring speed flaps 20 (APP)

A

80

24
Q

Approach speed, flaps 37.5

A

70-80

25
Q

Length for Long Nose and Short Nose

A

LN- 51ft 9 in
SN- 49ft 6 in

26
Q

Wing Span

A

65ft

27
Q

Tail Span

A

20 ft 8in

28
Q

Keel width

A

13ft 4in

29
Q

Float Length

A

31ft 10 in

30
Q

Rear Baggage Comp Mass

A

450 lbs ( including rear shelf)

31
Q

Rear Baggage Shelf Mass

A

150 lbs

32
Q

Nose Baggage Mass

A

LN- 300 lbs
SN- 200 lbs

33
Q

Max Floor Loading Main Cabin

A

200 lbs / sq ft

34
Q

Max loading Nose Baggage (long nose)

A

100 lbs / sq ft

35
Q

Max loading Rear Baggage

A

100 lbs / sq ft

36
Q

Cabin Baggage Area

A

200 lbs / sq ft

37
Q

Max G loadings

A

100/200 +3.21g & -1.5g
300 +3.17g & -1.5g

38
Q

Wind

A

Head wind 20kts (NL)
Tail wind 10kts (L)
Cross wind 17kts (NL)

39
Q

Engine Oil Capacities

A

Total - 2.3 USG
Usable -1.7 USG

40
Q

Fuel Capacity

A

Forward 1235 lbs (686 L)
Rear 1341 lbs (756 L)
Wing Tip 287 lbs (168 L)