Limitations Flashcards

(77 cards)

1
Q

Max ramp weight

A

85,000 lbs

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2
Q

Max takeoff weight

A

84,500 lbs

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3
Q

Max landing weight

A

75,100 lbs

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4
Q

Max Zero Fuel Weight

A

70,750 lbs

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5
Q

Minimum flight weight

A

45,000 lbs

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6
Q

Max aft cargo

A

3,740 lbs

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7
Q

Max aft cargo with wifi

A

3,650 lbs

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8
Q

Max forward cargo

A

1,700 lbs total split bin (850/850)

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9
Q

Flight time to suitable airport (Cargo Firex)

A

60 min

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10
Q

Bombardier Max Ops altitude (nice to know)

A

41,000 ft

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11
Q

Max Skywest Ops altitude

A

37,000 ft

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12
Q

Max takeoff and landing altitude

A

9,600 ft

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13
Q

Max temperature for takeoff/landing

A

ISA + 35°C

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14
Q

Minimum outside air temperature for takeoff

A

-40°C

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15
Q

Maximum tailwind

A

10 KTS

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16
Q

Vmo

A

335 KIAS

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17
Q

Mmo

A

.84 M (.82 RVSM)

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18
Q

Flaps 1

A

230 KIAS

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19
Q

Vfe 8

A

230 KIAS

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20
Q

Vfe 20

A

220 KIAS

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21
Q

Vfe 30

A

185 KIAS

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22
Q

Vfe 45

A

170 KIAS

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23
Q

Vlo extend

A

220 KIAS

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24
Q

Vlo retract

A

200 KIAS

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25
Vle
220 KIAS
26
Vtire
195 kts GS
27
Vadg Max deploy speed
Vmo/Mmo
28
Vb
280 KIAS
29
Mb
M .75
30
Vwiper Max ops
250 KIAS
31
When is anti-skid available after touchdown?
>35 kts or W-on-W +5 sec
32
What speed is anti-skid unavailable
10 kts
33
Max flap/slat altitude
15,000 ft
34
Minimum spoiler speed
Approach speed + 10
35
Minimum altitude for flight spoilers use (SkyWest limitation)
1000 ft HAT
36
Max ITT for start
815°C
37
N1 and N2 at idle after start
N1 - 20-25% | N2 - 55-65%
38
N1 and N2 APR Max power (nice to know)
``` N1 = 99.5% N2 = 99.4% ```
39
Ground engine start attempts
``` 90 sec ON - 10 sec OFF 90 sec ON - 10 sec OFF 90 sec ON - 5 min OFF 90 sec ON - 5 min OFF 90 sec ON - 5 min OFF ITT must be 120°C or less ```
40
Dry motor ground sequence
``` 90 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF ```
41
Total Usable Fuel - Pressure refueling
19,594 lbs
43
Minimum runway width
100 ft
44
Max fuel imbalance
``` 800 lbs (Same for all models) ```
44
Max passengers
DELTA Only: 76 total = 12 first, 64 coach
45
Max fuel imbalance FOR TAKEOFF
300 lbs
46
Minimum fuel required for a go-around (per wing)
600 lbs
46
Wing Span
81 ft, 4 in
47
Total usable fuel - gravity refueling
14,810 lbs
48
Max payload
23,350 lbs
49
Minimum Bulk Fuel Temp for Takeoff
-30°C
50
Minimum Bulk Fuel Temp in Flight
-40°C
51
Aircraft Length
119 ft 4in
52
Aircraft Tail Height
24ft 7in
53
Max Standing Water Depth for Takeoff/Landing
Takeoff = .50in / Landing .75in
54
Max Depth Slush Takeoff/Landing
``` Takeoff = .59in Landing = .88in ```
55
APU Minimum Temp for Start
-40°C
56
APU Max Operations Altitude
FL 390
57
APU - Max Start Altitude
FL370
58
APU Max altitude for bleed use
FL250
59
APU Max Altitude for engine restart
FL 210
60
Maximum Airspeed for APU door open and APU not operating
220 KIAS
61
Maximum Continuous DC TRU
120A
63
APU Generator
To FL 410 = 40kVA
64
APU starter duty cycle
``` 30 sec - 2 min 30 sec - 20 min 30 sec - 2 min 30 sec - 40 min * No more than 3 start attempts within 60 minutes ```
65
AFCS minimum use elevations
Takeoff = 600ft AGL, Non-precision/visual = 400ft AGL, Precision =
66
Engine Start (ground)
``` 90 sec ON - 10 sec OFF 90 sec ON - 10 sec OFF 90 sec ON - 5 min OFF 90 sec ON - 5 min OFF 90 sec ON - 5 min OFF ```
67
Dry Motor (ground)
``` 90 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF 30 sec ON - 5 min OFF ```
68
``` Engine Start (in flight): Max windmilling/starter-assisted cross-bleed relight altitude ```
FL 210
69
N1 requirement when setting thrust for takeoff
Crew must verify target N1 values are within +/- 1.0%. When thrust set for takeoff, target and N1 values must match.
70
Oil requirement after cold start
Thrust must remain at idle until oil psi in green - within 10 minutes
71
Single pack operations
FL 250
72
CPAM Pax O2
>= 14,000 ft cabin altitude
73
Max Depth Wet Snow for Takeoff/Landing
``` Takeoff = .59in Landing = .88in ```
74
Max Depth Dry Snow Takeoff/Landing
``` Takeoff = 3.0in Landing = 3.75in ```
75
700/900 - Can we dispatch on runways contaminated with ice with only one thrust reverser?
No
76
Minimum Fuel
2150 lbs
77
Emergency Fuel
1550 lbs