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Atlas/Southern 737-400 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max T/O and LDG Altitude

A

8400 or 9000 with CABIN ALT & TAKEOFF CONFIG (All SA Aircraft have these)

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2
Q

Turbulent Airspeed

A

264 KTS / .65 MACH

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3
Q

Max Operating Altitude

A

37000 ft

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4
Q

Max TO & LDG tailwind & Max demonstrated crosswind

A

10 kts / 35 kts

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5
Q

Do not operate HF radios during

A

Refueling

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6
Q

Max allowable on the ground altitude display for RVSM

A

CA & FO / CA or FO & field elevation

Sea level 40 ft 75 ft
5000 ft 75 ft
10,000 ft 75 ft

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7
Q

Max difference CA or FO & field elevation

A

75 feet

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8
Q

Max Taxi Weight

A

144000 or 150355 (499)

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9
Q

Max Takeoff Weight

A

143500 or 149914 (499)

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10
Q

Max landing weight

A

121000 or 123899 (499)

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11
Q

Max Zero Fuel Weight

A

113000 or 116844 (499)

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12
Q

Minimum Operating Weight

A

78000 (all)

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13
Q

Max cabin diff pressure

A

8.65

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14
Q

With engine bleeds on do not operate packs

A

On HIGH for takeoff, approach or landing

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15
Q

Flight with freight on main deck cargo compartment prohibited

A

without at least one pack operating

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16
Q

Use of aileron trim with autopilot engaged is

A

Prohibited

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17
Q

DO NOT ENGAGE AUTOPILOT for takeoff below

A

1000 feet

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18
Q

For single channel operation do not operate autopilot below

A

50 feet

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19
Q

Max glideslope angle

A

3.25 degrees

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20
Q

Min glideslope angle

A

2.5 degrees

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21
Q

Autoland may only be used with

A

Flaps 30 or 40 and both engines operative

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22
Q

Do not use VHF-2 with frequencies

A

120.000 or 120.005

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23
Q

Max Gen Drive Oil Temp

A

157 deg C

24
Q

Maximum Start EGT

A

725 deg C

25
Q

Max Takeoff EGT

A

930 deg C

26
Q

Max continuous EGT

A

895 deg C

27
Q

Maximum N1 RPM

A

106%

28
Q

Maximum N2 RPM

A

105%

29
Q

Max time limit for takeoff thrust

A

5 minutes

30
Q

Maximum Oil Temp

A

160-165 deg C for 15 minutes

31
Q

Maximum Continuous Oil Temp

A

160 deg C

32
Q

Minimum Oil pressure

A

13 psi

33
Q

Engine Ignition

A

Continuous ignition must be on during takeoff, landing and engine anti ice operation.`

34
Q

PMC Computers

A

Both must be either OFF or ON for takeoff

35
Q

intentional selection of reverse thrust in flight

A

PROHIBITED

36
Q

Pneumatic pressure

A

minimum 30 psig @ sea level decreasing 1/2 psi per 1000 ft above sea level.

37
Q

APU Limitations

A

APU Bleed & Electrical 10,000 ft
APU Bleed only 17,000 ft
APU Electrical load only 35,000 ft

38
Q

APU Max Start EGT

A

760 deg C

39
Q

APU Max Continuous EGT

A

710 deg C

40
Q

APU can operate up to

A

37,000 ft

41
Q

APU Start limitations

A

5 minutes between 2nd and 3rd attempt

one hour after the third attempt.

42
Q

Maximum Flap Extension

A

20,000 ft

43
Q

In flight do not extend SPEED BRAKE beyond

A

Flight Detent

44
Q

Avoid (flight controls)

A

rapid and large alternating control inputs, especially in combination with large changes in pitch roll, or yaw as they may result in structural failure at any speed, including below Va

45
Q

Do not deploy speed brakes in flight below

A

at radio altitudes below 1000 ft

46
Q

Alternate flap duty cycle, after releasing ALTERNATE FLAPS position switch allow –>

A

15 seconds (intermittent) or 5 minutes after a complete extend / retract cycle.

47
Q

Do not use the EGPWS for

A

Navigation

48
Q

Do not operate weather radar

A

in a hangar or within 50 feet of personnel or a fuel spill

49
Q

Maximum fuel temperature

A

49 deg C

50
Q

Minimum fuel temperature

A

fuel freeze point +3 or -45 whichever is higher

51
Q

fuel imbalance

A

must be scheduled to zero

52
Q

random fuel imbalance

A

1000 lbs for taxi, takeoff, flight or landing

53
Q

main tanks 1 and 2 must be scheduled to full

A

if center tank contains more than 1000 lbs

54
Q

do not apply brakes

A

until after touchdown

55
Q

Main cargo compartment air supply shutoff / Main deck cargo compartment smoke detector system / Secondary main landing gear position indicating system

A

functionally operate the main cargo compartment air supply shutoff valve to ensure proper operation prior to each flight or series of flights by same crew on same day

56
Q

Main deck cargo door

A

do not open main deck cargo door in actual or anticipated winds exceeding 45 knots

57
Q

aircraft in not to be taxied, towed of jacked unless

A

MAIN DECK CARGO DOOR is in fully closed and latched position

Atlas/Southern 737-400 (11 decks)

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