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SAI 737 > Limitations > Flashcards

Limitations Flashcards

1
Q

MAX TAXI WEIGHT

A

144,000 lb

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2
Q

N311GT

MAX TAXI WEIGHT

A

150,355 lb

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3
Q

Max Takeoff Weight

A

143,500 lb

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4
Q

N311GT

MAX TAKEOFF WEIGHT

A

149,914 lb

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5
Q

MAX LANDING WEIGHT

A

121,000 lb

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6
Q

N311GT

MAX LANDING WEIGHT

A

123,899 lb

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7
Q

MAX ZERO FUEL WEIGHT

A

113,000 lb

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8
Q

N311GT

MAX ZERO FUEL WEIGHT

A

116,844 lb

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9
Q

MIN OPERATING WEIGHT

A

78,000 lb

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10
Q

N311GT

MIN OPERATING WEIGHT

A

78,000 lb

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11
Q

Use of aileron trim with__________ ___________ is prohibited.

A

Autopilot Engaged

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12
Q

Do not engage auto pilot on takeoff below ________ _________ AGL

A

Below 1000 feet

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13
Q

For single channel ops during approach, the autopilot shall not remain engaged below ________ _________ AGL

A

50 feet AGL

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14
Q

Auto-land capability can only be used with flaps _____or_______ with both ___________ ___________

A

30 or 40. Engines Operative

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15
Q

MAX ENGINE START EGT

A

725 C

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16
Q

Intentional selection of reverse thrust in flight is __________________

A

Prohibited

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17
Q

APU

BLEED PLUS ELECTRICAL MAX ALT

A

10,000 feet

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18
Q

APU

BLEED AIR ONLY MAX ALT

A

17,000 feet

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19
Q

APU

ELECTRICAL MAX ALT

A

35,000 feet

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20
Q

APU

MAX OPERATING ALT

A

37,000 feet

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21
Q

APU
If there are multiple aborted start attempts, ___________minutes cooling is required between second and third start attempt. A wait of _________ ___________ after third start attempt.

A

Five

One hour

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22
Q

Max flap extension altitude is ___________ feet pressure altitude

A

20,000

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23
Q

Avoid _______ and _____________ _______________ ______________ ______________, especially in combination with large changes in pitch, roll, or yaw. As they may result in structural failure at any speed ___________ ____________ _____

A

Rapid and Large Alternating control inputs

Including below Va

24
Q

When extending and retracting flaps with the ALTERNATE FLAPS position switch, allow _______ ______________ after releasing the ALTERNATE FLAPS switch before moving the switch again to avoid damage to the alternate flaps motor clutch.

A

15 seconds

25
Q

Regarding Alternate Flaps
After a completed extend/retract cycle, ie ____ to _____ and ________ to _______ allow ________ __________ cooling before attempting another extension.

A

0 to 15 and back to 0

5 minutes

26
Q

Do not operate weather radar in the _______________ or within _________ __________ of any personnel Or fuel spill

A

Hanger,

50 feet

27
Q

Lateral imbalance between main tank 1 and 2 must be scheduled to ___________

A

Zero

28
Q

Random fuel imbalance must not exceed _____________ lbs for taxi, takeoff, flight or landing.

A

1000 lbs

29
Q

Main tanks must be scheduled to be full if center tank contains more than _____________lbs fuel

A

1000 lbs

30
Q

Do not open main deck cargo door in actual or anticipated winds exceeding ____________ knots

A

45

31
Q

Max glideslope angle __________degrees

A

3.25 degrees

32
Q

Minimum Glideslope angle is ____________ degrees

A

2.5 degrees

33
Q

Max takeoff and landing altitude_______________ ________________ ____________Altitude
With “Cabin Altitude” and “Takeoff Config” installed and operative
_____________ ___________ ______________ Altitude

A

8,400 feet pressure altitude

9,000 feet pressure altitude

34
Q

Max aircraft operating altitude ____________ feet

A

37,000

35
Q

Max Takeoff and landing tailwind component

A

10 knots

36
Q

Demonstrated takeoff and landing crosswind component

A

35 knots

37
Q

Do not operate HF radios during __________________

A

Refueling

38
Q

Turbulent Airspeed

A

264 KIAS / .65M

39
Q

Max allowable in-flight difference between Altimeters Captain and FO for RVSM

A

200 feet

40
Q

Max allowable On-Ground difference between Altimeters Captain or FO and Feild Elevation for RVSM

A

75 feet

41
Q

Max cabin differential

A

8.65 psi

42
Q

The use off frequency _____.000 and 120._____ is prohibited on which comm radio?

A

120.000
120.005
VHF #2

43
Q

Max Generator drive temp

A

157C

44
Q

Max Engine N1

A

106%

45
Q

Max Engine Takeoff EGT

A

930C

46
Q

Max Engine Continuous EGT

A

895C

47
Q

Min Engine Oil Pressure

A

13 psi

48
Q

Cont Ignition must be used during _________, ___________ ,and ______-_______ Operations

A

Takeoff
Landing
Anti-Ice

49
Q

Max APU EGT

A

760C

50
Q

Max APU Continuous EGT

A

710C

51
Q

Min fuel temp

A

Freeze point +3C or -45C whichever is higher

52
Q

Max fuel temp

A

49C

53
Q

For use of Electric Hydraulic Pump the respective side fuel main tank must contain a minimum of_________LBS

A

1675 lbs

54
Q

The Main wing tanks hold ___,________lbs each

A

10,043 lbs

55
Q

The Center Tank holds ____,__________ lbs

A

15,497 lbs

56
Q

Total Fuel load is ______,______________ lbs

A

35,583 lbs

SAI 737 (3 decks)

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