Limitations 700/900 Flashcards

(67 cards)

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
Vfe 45
170 KIAS
26
Vlo ext
220 KIAs
27
Vlo RET
200 KIAS
28
Vle
220 KIAS
29
Vtire
182 K GS | 195 K GS
30
V ADG Deploy Max
Vmo / Mmo
31
Vb
280 KIAS
32
Mb
.75 M
33
Vwiper ops max
250 KIAS
34
Anti Skid
>35 kts or WOW +5 sec
35
Ant Skid inop below
10 kts
36
SLATS / FLAPS
15,000 ft
37
Min Spoiler speed
Vref +10
38
Min ALT Spoilers
300 ft
39
N2 IDLE
55 - 65% | 55 - 65%
40
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 ```
41
DRY Motoring 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 ```
42
Usable Fuel: | L Main
7,492 lbs
43
Usable Fuel: | R Main
7,492 lbs
44
Usable Fuel: | Center
4,610 lbs
45
Usable Fuel: | Total
19,594 lbs
46
Max Imbalance
800 lbs
47
Max Imbalance for T/O
300 lbs
48
Min for GA per wing
600 lbs
49
Min Temp T/O
+5 C
50
Main Gen
to 41,000 ft: 40 KVA
51
APU Gen
to 41,000 ft: 40 KVA
52
GND Ops DC ONLY
5 min
53
Precision approach: >3.5 and < or = 4.0 min use alt
120 ft
54
Precision Approach: | Single engine min use alt
110 ft
55
Press max diff
8.7 PSI
56
Max neg diff
- 0.5 PSI
57
Single Pack Ops to
FL 310 | FL 250
58
PRESS Note:
Use of the EMER DEPRESS switch above 15,000 feet is prohibited Limit climb to less than 1500 FPM above FL300
59
APU Max Start ALT
37,000 ft
60
APU Max Alt bleed use
25,000 ft
61
APU alt engine start
21,000 ft
62
APU Start Note:
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
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
3 minutes - 1 hour
64
Bulk Fuel Take Off Limit and Freezing point
-30 C / -40 C
65
__________ climb speed profile above ________ - ________________.
Maximum - 10,000' - 290 KIAS to .74 M
66
Maximum authorized alttitude _________
FL390
67
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 _____________.
running - N1 - EICAS - equal to or greater than - takeoff report