Limitations Flashcards

(37 cards)

1
Q

What is the Ramp weight

A

36,500

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2
Q

What is the max take-off weight

A

36,300

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3
Q

Max landing weight

A

34,500

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4
Q

Max zero fuel weight

A

32,000

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5
Q

Manuevering load limit with flaps retracted

A

+ 2.5 g and - 1 g

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6
Q

Manuevering load limit with flaps extended

A

+ 2 g and 0 g

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7
Q

Maximum operating altitude

A

25,000 ft ASL

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8
Q

Maximum operating altitude for take-off and landing

A

10,000 ft ASL

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9
Q

Maximum runway slope

A

+ 2% uphill and -2% downhill

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10
Q

Maximum tailwind component

A

10 kts

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11
Q

Maximum crosswind component

A

36 kts

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12
Q

Ambient temperature limits

A

+48.9 C or ISA +35 C whichever is lower Max and -54 C minimum

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13
Q

Manuevering speed Va

A

164 KIAS

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14
Q

Flap Extended Speed Vfe

A

5 and 15 Flaps 148 KIAS 35 Flaps 130 KIAS

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15
Q

Maximum operating speed Vmo

A

SL 242 KIAS to 25,000’ 207 KIAS

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16
Q

Landing gear extended speed Vle

17
Q

Landing gear operating speed Vlo - can extend the gear

18
Q

Rough Air Speed

19
Q

Alternate gear extension speed

20
Q

Maximum altitude for airstart

21
Q

Automatic take-off power control system (uptrim)

22
Q

MTOP - Max take-off power

A

111% TQ (5 min), 800 C T6, 102.7 Nh, 1212 Np, 55-65 PSI Oil, 45-115 C Oil temp

23
Q

NTOP - Normal take-off power

A

99.5%, 770 C T6, 101 Nh, 1212 Np, 55-65 PSI Oil, 45-115 C Oil temp

24
Q

MCP - Max continuous power

A

97.5%/1212 Np or 114.2% 1024 Np, 800 C T6, 102.7 Nh, 55-65 PSI Oil, 45-115 C Oil temp

25
Engine start temperature limits
840-900 C for 12 seconds, 900-950 5 for 5 seconds
26
Engine start max oil pressure
200 PSI
27
Engine start min oil temperature
-40 C
28
Max transient conditions which are limited to 20 seconds
125% TQ, 840 C T6, 103.7 Nh, 1320 Np, 200 PSI Oil, 125 C Oil temp
29
Max Torque for reverse
90%
30
Max Np for reverse
1212 RPM
31
Max Nh for reverse
101 RPM
32
What is propellor prohibited range
500-780 RPM
33
Maximum tire speed
165 KIAS
34
Maximum altitude with landing gear and flaps extended
15,000' ASL
35
Normal cabin pressure differential limit
5.5 +/- .3 PSI
36
Maximum cabin pressure differential
5.95 PSI
37
Maximum cabin altitude
8,000'