Limitations 700/900 Flashcards

1
Q

L(R) Start abort Msg, Hot Start

A

Affected Thrust Lever - Shut Off
Dry Motor - until ITT reduced below 120 C, respecting starter time limit
Affected ENG STOP - STOP

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2
Q

Stab Trim Runaway

A

Control wheel - assume manual control and override runaway

STAB TRIM DISC - select

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3
Q

Max Ramp Weight

A

75,250 lbs

85,000 lbs

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4
Q

Max T/O weight

A

75,000 lbs

84,000 lbs

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5
Q

Max T/O weight Delta and Alaska 700s

A

74,999 lbs

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6
Q

Max Landing weight

A

67,000 lbs

75,100 lbs

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7
Q

Max Zero Fuel weight

A

62,300 lbs

70,750 lbs

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8
Q

Min flight weight

A

42,000 lbs

45,000 lbs

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9
Q

Max AFT cargo

A

3,740 lbs

3,740 lbs

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10
Q

Max AFT Cargo, WIFI 700 and 900

A

3,650 lbs

3,650 lbs

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11
Q

Max AFT Cargo Alaska 700s

A

4,375 lbs

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12
Q

Max FWD Cargo

A

1,000 lbs

1,700 lbs. Total split bin 850/850

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13
Q

Max ops alt SkyWest

A

39,000 ft

39,000 ft

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14
Q

Max T/O and Lnd

A

9,600 ft

9,600 ft

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15
Q

Max Temo T/O and LND

A

ISA +35 C

ISA +35 C

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16
Q

Min Temp T/O

A
  • 40 C

- 40 C

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17
Q

RWY Slope

A

+/- 2%

+/- 2%

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18
Q

Max Tailwind

A

10 kts

10 kts

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19
Q

Vmo

A

335 KIAS

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20
Q

Mmo

A

.85 (.83 RVSM)

.84 (.82 RVSM)

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21
Q

Flap 1

A

230 KIAS

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22
Q

Vfe 8

A

230 KIAS

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23
Q

Vfe 20

A

230 KIAS

220 KIAS

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24
Q

Vfe 30

A

185 KIAS

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25
Q

Vfe 45

A

170 KIAS

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26
Q

Vlo ext

A

220 KIAs

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27
Q

Vlo RET

A

200 KIAS

28
Q

Vle

A

220 KIAS

29
Q

Vtire

A

182 K GS

195 K GS

30
Q

V ADG Deploy Max

A

Vmo / Mmo

31
Q

Vb

A

280 KIAS

32
Q

Mb

A

.75 M

33
Q

Vwiper ops max

A

250 KIAS

34
Q

Anti Skid

A

> 35 kts or WOW +5 sec

35
Q

Ant Skid inop below

A

10 kts

36
Q

SLATS / FLAPS

A

15,000 ft

37
Q

Min Spoiler speed

A

Vref +10

38
Q

Min ALT Spoilers

A

300 ft

39
Q

N2 IDLE

A

55 - 65%

55 - 65%

40
Q

Engine Start Ground

A
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
41
Q

DRY Motoring Ground

A
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
42
Q

Usable Fuel:

L Main

A

7,492 lbs

43
Q

Usable Fuel:

R Main

A

7,492 lbs

44
Q

Usable Fuel:

Center

A

4,610 lbs

45
Q

Usable Fuel:

Total

A

19,594 lbs

46
Q

Max Imbalance

A

800 lbs

47
Q

Max Imbalance for T/O

A

300 lbs

48
Q

Min for GA per wing

A

600 lbs

49
Q

Min Temp T/O

A

+5 C

50
Q

Main Gen

A

to 41,000 ft: 40 KVA

51
Q

APU Gen

A

to 41,000 ft: 40 KVA

52
Q

GND Ops DC ONLY

A

5 min

53
Q

Precision approach:
>3.5 and < or = 4.0
min use alt

A

120 ft

54
Q

Precision Approach:

Single engine min use alt

A

110 ft

55
Q

Press max diff

A

8.7 PSI

56
Q

Max neg diff

A
  • 0.5 PSI
57
Q

Single Pack Ops to

A

FL 310

FL 250

58
Q

PRESS Note:

A

Use of the EMER DEPRESS switch above 15,000 feet is prohibited
Limit climb to less than 1500 FPM above FL300

59
Q

APU Max Start ALT

A

37,000 ft

60
Q

APU Max Alt bleed use

A

25,000 ft

61
Q

APU alt engine start

A

21,000 ft

62
Q

APU Start Note:

A

Do note perform more than three starts/start attempts in one hour.
a two minute delay must be observed between cranking attempts to allow for cooling of starter and starter contactor and for APU drainage.

63
Q

For airplane operation in excess of 36 hours (without engine oil tank servicing) the engine oil level must be checker within __________ to ________ of every engine shutdown

A

3 minutes - 1 hour

64
Q

Bulk Fuel Take Off Limit and Freezing point

A

-30 C / -40 C

65
Q

__________ climb speed profile above ________ - ________________.

A

Maximum - 10,000’ - 290 KIAS to .74 M

66
Q

Maximum authorized alttitude _________

A

FL390

67
Q

The flight crew must verifiy (with the engines __________) that the target ____ displayed on ___________, following input of the assumed temperature, is _________________________ the appropriate N1 value contained in the reduced thrust section of the _____________.

A

running - N1 - EICAS - equal to or greater than - takeoff report