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Southern Air 737-800 PC Prep > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway slope

A

+/- 2%

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2
Q

Maximum takeoff and landing tailwind component

A

10 knots

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3
Q

Maximum demonstrated T/O and Landing crosswind

A

33 kts

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4
Q

Maximum Speeds

A

Observe VMO Pointer and gear / flap placards

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5
Q

Maximum flight operational latitude

A

82N and 82S

Except for the region between 80W and 130W longitude, the maximum flight operating latitude is 70N, and the region between 120E and 160E longitude, the maximum flight operating latitude is 60S.

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6
Q

Maximum operating altitude

A

41,000 ft

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7
Q

Maximum Takeoff and Landing Altitude

A

8,400 ft

for N5227A
13,500 ft

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8
Q

How often do we verify that an operational check of the flight deck door system has been accomplished?

A

Once each flight day

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9
Q

Severe Turbulent Air Penetration Speed

What about during cruise?

A

280KIAS or .76M (whichever is lower)

*Note: During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure

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10
Q

On revenue flights what must be installed regarding L1 Door

A

The escape slide retention bar (girt bar), during taxi, takeoff, and landing

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11
Q

What must not be operated during refueling operations

A

HF radios

*Do not operate HF radios during refueling operations.

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12
Q

Do standby altimeters meet altimeter accuracy requirements of RVSM airspace?

A

No

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13
Q

Max allowable in-flight difference between captain and FO altitude display for RVSM

A

200 feet

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14
Q

Maximum allowable on-the-ground altitude display differences for RVSM operations between Captain and FO?

A

Sea level to 5,000 ft = 50 ft

5,000 ft to 10,000 ft = 60 ft

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15
Q

Weight Limitations Max Taxi

A

174,700 lbs

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16
Q

Weight Limitations Max Takeoff

A

174,200 lbs*

*may be further restricted by takeoff, enroute, and landing performance.

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17
Q

Weight Limitations Max Landing

A

146,300 lbs*

*may be further restricted by field length or climb limit

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18
Q

Weight Limitations Max Zero Fuel

A

138,300 lbs

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19
Q

Weight Limitations Min Operating

A

80,800 lbs

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20
Q

Max differential pressure

A

9.1 PSI

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21
Q

With either one or both engine bleed air switches ON, do not operate the air conditioning packs in

A

HIGH for takeoff, approach, or landing.

*Note: The fire protection Non-Normal procedures take precedence over the statement regarding no air conditioning pack in HIGH during takeoff, approach or landing. The SMOKE or FUMES REMOVAL checklists and CARGO FIRE checklists require the Operating PACK switch(es) HIGH. Switch(es) need to be placed in HIGH in order to increase ventilation for smoke removal.

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22
Q

Use of Aileron trim with the autopilot engaged is

A

Prohibited

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23
Q

Do not engage the autopilot for takeoff below what ALT

(N5227A) - Do not use the autopilot below _____ at airport pressure altitudes above ______.

A

400 feet AGL

100’ RA, 8,400’ PA

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24
Q

For single channel operating during approach, when shall the autopilot be disengaged

A

50 feet AGL

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25
Q

MAX Wind Component for Autoland

A

Headwind: 25kts
Tailwind: 10kts
Crosswind: 20kts
Crosswind CAT 2/3: 15kts

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26
Q

MAX and MIN glideslope angles for Autoland

A

3.25 to 2.5 degrees

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27
Q

Autoland capability may only be used with (flap and engine requirements)

Autoland capability may only be used N5227A?

A

flaps 30 or 40 and both engines operative.

to runways at or below 8,400 ft pressure altitude.

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28
Q

When can you not use LVL Change on final approach (APP)?

A

Do not use on final approach below 1,000 AFE

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29
Q

Do not use what VHF # for ATC communications with ACARS operational?

A

VHF-3

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30
Q

ACARS is limited to the transmission and receipt of messages that will not create an unsafe condition if the message is improperly received, such as these conditions:

A
  • the message or parts of the message are delayed or not received
  • the message is delivered to the wrong recipient
  • the message content may be frequently corrupted

Note: Pre-Departure Clearance, Digital ATIS (Automatic Terminal Information Service), Weight and Balance, and Takeoff Data messages can be transmitted and received over ACARS if they are verified per approved operational procedures.

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31
Q

Use what VHF # for primary communications the ground?

A

VHF-1

32
Q

Where is the VHF-1 radio connected?

A

to the top of the fuselage antenna

33
Q

Engine limit display markings (What colors)

A 
Red = maximum and minimum limits
Amber = caution limits
34
Q

Maximum time limit for takeoff thrust

A

5 minutes

35
Q

Engine Ignition must on AUTO/CONT for what phases?

A

T/O, Landing, Anti-ice operation and operation in heavy rain

36
Q

Operation with Assumed temperature reduced takeoff thrust is not permitted with what INOP?

A

anti-skid inoperative

37
Q

When is intentional selection of reverse thrust is prohibited?

A

in flight

38
Q

APU Max config ALT’s

A

APU bleed + electric load = 10,000 ft (In Flight), 15,000 ft (Ground Only)
APU bleed = 17,000 ft
APU Electrical Load = 41,000 ft

39
Q

Engine Normal Starter duty cycle

A

Multiple consecutive start attempts are permitted, each start attempt limited to 2 minutes of starter usage

minimum of 10 seconds is needed between start attempts

40
Q

Engine Extended Engine Motoring

A

Starter usage is limited to 15 mins for the first two extended engine motorings. A minimum of 2 minutes is needed between each attempt.

For the third and subsequent extended motorings, starter usage is limited to 5 minutes. A minimum of 10 minutes is needed between each attempt

41
Q

APU bleed valve must be closed when?

A
  1. Ground air connected and isolation valve is open
  2. Engine no.1 bleed valve open
  3. Isolation and engine no. 2 bleed valve open

Note: APU bleed valve may be open during engine start, but avoid engine power above idle

42
Q

After 3 consecutive APU aborted start attempts, how long is the cooling period required?

A

15 minute cooling period

43
Q

The max alt for flaps extended is?

A

20,000 feet

44
Q

Holding in icing conditions with flaps extended is?

A

Prohibited

45
Q

In flight, do not extended the speed brakes past what point?

A

Flight Detent

46
Q

Rapid and large alternating control inputs may result in what?

A

structural failure at any speed, including below VA
(Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.)

47
Q

Do not deploy speedbrakes in flight below what ALT?

A

at radio altitudes less than 1,000 ft

48
Q

Alternate Flap Duty Cycle

A

when extending or retracting flaps with the ALTERNATE FLAPS position switch, allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to ALTERNATE FLAP motor clutch

After a complete extend and retract cycle 0-15 and back to 0, allow 5 mins for cooling before trying again

49
Q

All flight operations based on magnetic heading or magnetic track angle are prohibited where?

Where do we find this information?

A

in geographic areas where the installed IRS MagVar table errors are greater than 5 degrees.

Refer to AFM Normal Procedures/Intertial Reference System section

50
Q

Do not use this display for navigation

A

The terrain display

51
Q

When can we NOT use the look-ahead terrain alerting and terrain display functions

A

Within 15 nm of takeoff, approach, or landing at an airport not contained in the GPWS terrain database.

52
Q

Avoid WX radar operation where/when?

A
  • In a hanger (no longer listed: within 50ft of fueling operations or fuel spill)
  • when personnel are within the area normally enclosed by the aircraft nose radome.

The hangar recommendation does not apply to the weather radar test mode.

53
Q

If a fuel pump circuit break trips, can you reset it?

What about if in flight? More than once?

What is the cooling period?

A

NO

Yes, if directed by a non-normal checklist, but it is not recommended. A tripped circuit breaker may be reset once, after a short cooling period (approximately 2 minutes), if in the judgement of the captain, the situation resulting from the circuit breaker trip has a significant adverse effect on safety.

54
Q

The Use of what Fuel is prohibited?

A

Jet B and JP-4

55
Q

Maximum Tank fuel Temp

A

49 degrees Celsius

56
Q

Inflight tank fuel temp must be what in flight?

Does the use of Fuel System Icing Inhibitor additives change the minimum fuel tank temperature limit?

A

must be maintained at least 3 degrees C above the freezing point of the fuel used or -43C whichever is higher

No, the use of Fuel System Icing Inhibitor additives does NOT change the minimum fuel tank temperature limit

57
Q

What fuel is allowed?

A

JET A, JET A-1, JP-5, JP-8

58
Q

Intentionally dry running the center tank fuel pump (low pressure light illuminated) is?

A

Prohibited

59
Q

Maximum scheduled lateral fuel imbalance between tanks 1 and 2 is?

A

0 lbs

60
Q

Random/transient fuel imbalance is ?

A

Must not exceed 1,000 lbs for Taxi, T/O, Flight, Landing

61
Q

Main tanks must have how much fuel if the center tank contains more than _____?

A

Full, 1,000 lbs

62
Q

Do not apply brakes until

A

after touchdown

63
Q

Do not open the main deck cargo door in actual or anticipated winds exceeding?

A

45 knots

64
Q

Aircraft is not to be taxied, towed, or jacked unless ?

A

the MAIN DECK CARGO DOOR is in the fully closed and latched position.

65
Q

With either one or both engine bleed air switches ON, do not operate what?

What takes precedence?

A

do not operate the air conditioning packs in HIGH for takeoff, approach, or landing.

The fire protection Non-Normal procedures take precedence over the statement above. The SMOKE or FUMES REMOVAL checklists and CARGO FIRE checklists require the Operating PACK switch(es) HIGH. Switch(es) need to be placed in HIGH in order to increase ventilation for smoke removal.

66
Q

Flights predicated on the use of which HF frequencies are prohibited for N5227A, N5233A, and N5237A?

A

29.489 and 29.490 MHz.

67
Q

What CDS software do all Southern 737-800 aircraft have installed?

Why does it matter?

A

BP15 and FMCsoftware U13.0

There are 6 runways that may blank all six display units if they are selected in the FMC ARRIVALS page.

68
Q

If an amber caution light illuminates during MASTER CAUTION recall, but extinguishes after MASTER CAUTION reset, what do we need to do?

A

Nothing. Completion of the associated checklist is not required.

69
Q

Do not use ________ below _____ feet radio altitude at airport pressure altitudes above ______ feet.

A

autopilot, 100’ RA, PA above 8,400 (N5227)

70
Q

HF radios must not be operated when?

A

During refueling operations

71
Q

Maximum allowable on-the-ground altitude display differences for RVSM operations between Captain or FO and Field Elevation?

A

75 feet

72
Q

Use of _______ with the autopilot engaged is prohibited?

A

Aileron trim

73
Q

If the anti-skid is inoperative, what kind of takeoff is not permitted?

A

Operation with Assumed temperature reduced takeoff thrust

74
Q

Can the APU bleed valve may be open during engine start?

A

Yes, but avoid engine power above idle.

75
Q

With the altimeters referenced to QFE, what is prohibited?

A
  • The use of VNAV or LNAV

- The use of the Vertical Situation Display (VSD)

76
Q

If the option for QFE altitude reference selection is not installed in the FMS, what is prohibited?

A

QFE operations

77
Q

When must a QFE altitude reference for the PFDs be selected?

A

whenever the QFE is used instead of QNH

Southern Air 737-800 PC Prep (3 decks)

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