LIMITATIONS Flashcards
Where is the Datum located in Short Nose?
Approx 6” forward of the nose cone fairing
Where is the Datum located in Long Nose?
Approx 21” aft of the tip of the nose cone fairing
Where is the CG Range T/O and LDG (all series @ all weight on wipline floats)
Forward 207.74 in (25% MAC)
Aft 213.20 in (32% MAC)
Ref datum 60” forward of front fuselage bunk head
Mass Limitations for 100/200
M. T/O- 11,600 lbs
M. LDG- 11,600 lbs
M. 0 Fuel- 11,400 lbs
Mass limitations for 300
M. T/O- 12,500 lbs
M. LDG- 12,500 lbs
M. 0 Fuel- 12,300 lbs
VMO for 100/200
158 up to 10,000ft
Vp/Va/Vb for 100/200
129
Vmc flaps 10 for 100/200
67
Vmc flaps 20 for 100/200
67
VMO for 300
158 decrease by 1 every 1000ft
Vp/Va/Vb for 300
135
Vmc flaps 10 for 300
70
Vmc flaps 20 for 300
67
VFE flaps 0-20 for 100/200
100
VFE flaps 20-37.5 for 100/200
85
VFE flaps 0-10 for 300
102
VFE flaps 10-37.5 for 300
95
Vx
82
Vy
90
Vyse flaps 10
86
Vno flaps 0
120
minimum manoeuvring speed flaps 0
100
minimum manoeuvring speed flaps 10
90
minimum manoeuvring speed flaps 20 (APP)
80
Approach speed, flaps 37.5
70-80
Length for Long Nose and Short Nose
LN- 51ft 9 in
SN- 49ft 6 in
Wing Span
65ft
Tail Span
20 ft 8in
Keel width
13ft 4in
Float Length
31ft 10 in
Rear Baggage Comp Mass
450 lbs ( including rear shelf)
Rear Baggage Shelf Mass
150 lbs
Nose Baggage Mass
LN- 300 lbs
SN- 200 lbs
Max Floor Loading Main Cabin
200 lbs / sq ft
Max loading Nose Baggage (long nose)
100 lbs / sq ft
Max loading Rear Baggage
100 lbs / sq ft
Cabin Baggage Area
200 lbs / sq ft
Max G loadings
100/200 +3.21g & -1.5g
300 +3.17g & -1.5g
Wind
Head wind 20kts (NL)
Tail wind 10kts (L)
Cross wind 17kts (NL)
Engine Oil Capacities
Total - 2.3 USG
Usable -1.7 USG
Fuel Capacity
Forward 1235 lbs (686 L)
Rear 1341 lbs (756 L)
Wing Tip 287 lbs (168 L)
