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737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway slope

A

+/- 2 %

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2
Q

Max tailwind

A

15kts

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3
Q

Max Operating Altitude?

A

41000’

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4
Q

Max Alt TO/Land

A

8400’ PA

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5
Q

Max engine out Altitude with ViaSat installed?

A

Applicable only to airplanes fitted with​ ViaSat​ inflight connectivity systems: The ​FMC-derived Engine-Out Cruise Maximum Altitude is required​ to​ be​ reduced by ​400ft

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6
Q

Overwing exit limitation?

A

Installation of handle covers on the overwing exits must be verified prior to​ ​departure whenever passengers are carried.

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7
Q

Narrow Runway Operations

A

Operation on Narrow Runways ​(Widths less than 45m, but not less than 30m)​

Visibility​
The runway centerline shall be clearly​ visible in the prevailing conditions.​
Airplane Systems​
The dispatch​ from / to runways less than 45m wide is​ not allowed in the case of ​nose gear steering inoperative or one thrust​ reverser inoperative.​ If an alternate ​airport is available with a runway at least 45m wide, diversion to that alternate ​shall be performed in case of jammed or restricted flight​ controls,
trailing edge ​flap asymmetry,
leading edge flap/slat asymmetry,​
or loss of system A​ or B ​hydraulics.

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8
Q

Turb pen speeds:

A

Severe Turbulence Air Penetration speed is 280​ KIAS/.76 Mach, whichever is ​lower. Applicable to Climb and Descent only.
During cruise, refer to SP.16, Severe ​Turbulence​ Supplementary Procedure

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9
Q

HF

A

Do not operate HF radios during​ refueling​ operations

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10
Q

Girt Bar

A

On revenue flights, the escape slide retention bar (girt bar) must​ be installed​ ​during​ taxi, takeoff and landing

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11
Q

Ground​ Wind Limits for all​ Doors

A

40kt while opening or closing​
65kt while open

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12
Q

Standby Altimeters (RVSM)

A

Standby altimeters​ do​ not meet altimeter accuracy​ requirements​ of RVSM ​airspace.

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13
Q

The maximum allowable in-flight difference between Captain and First Officer ​altitude displays for RVSM​ operations is

The maximum allowable on-the-ground altitude​ display differences for RVSM ​operations are

A

200’

Field Elevation 0’-5000
C-FO 50’, C OR FO and Field 75’

5001’-10000’
60’ and 75’

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14
Q

MLW

A

66360kg all rego’s

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15
Q

Weights

A
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16
Q

maximum cabin differential pressure (relief​ valves) is

A

9.1psi

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17
Q

Engine Bleeds

A

With either one or both​ engine bleed air switches ON, do​ not operate the air ​conditioning packs in HIGH for takeoff, approach or landing.​

Note:​ The fire protection Non-Normal procedures takes precedence over the ​statement regarding no​ air conditioning​ pack in HIGH during takeoff, ​approach, or landing. The CARGO FIRE​ and SMOKE/ FUMES ​REMOVAL​ 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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18
Q

Aileron Trim

#

A

Use of aileron trim with​ the autopilot​ engaged is prohibited.

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19
Q

AP engage TO?

A

Do not engage the autopilot for takeoff below​ 400ft AGL.

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20
Q

Single Channel AP approach?

A

For single channel operation during approach, the autopilot shall not​ remain ​engaged below​ 50ft​ AGL

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21
Q

Maximum allowable wind​ speeds when​ ​landing weather minima are predicated​ on autoland operations

A

Airplanes operating with FAA​ Rules:​ Maximum allowable wind​ speeds when​ ​landing weather minima are predicated​ on autoland operations:​
•​ Headwind 25kt​
•​ Crosswind 20kt​
•​ Tailwind​ 15kt

22
Q

Maximum and minimum glideslope​ angles for autoland

A

Maximum and minimum glideslope​ angles for autoland are 3.25 degrees and​ 2.5 ​degrees respectively

23
Q

Autoland Allowable Config:

A

Autoland​ capability may​ only​ be used with flaps 30 or 40​
and both​ engines ​operative

24
Q

Level Change

A

Do not use LVL​ CHG on final approach below 1,000ft AFE

25
Q

Prohibited HF frequencies:

A

VH-VXA -VH-VXU, VH-VYA -VH-VYL​
Flights predicated on the use of the following HF frequencies are prohibited:​
•​ 29.489Mhz​
•​ 29.490Mhz

26
Q

ACARS:

A

The 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 the ​following​ conditions:​
•​ the message or parts of the message are delayed or not received,​
•​ the message is delivered​ to the wrong recipient, or​
•​ the message content may be frequently corrupted.​
•​ However,
Pre-Departure Clearance,
Digital Automatic Terminal ​Information Service,
Oceanic Clearances,
Weight and Balance
and ​Takeoff Data messages can be transmitted and received over ACARS if ​they are verified per approved operational procedures

27
Q

Primary Ground VHF?

A

Use the VHF radio connected​ to the top of fuselage antenna for primary ATC ​communications on the ground

28
Q

Engine Limits

A

Maximum and minimum​ limits are red.​
Caution limits are amber

29
Q

Engine Ignition?

A

Engine ignition​ must be on​ for:​
•​ takeoff​
• landing​
•​ operation in heavy​ rain​
•​ anti-ice operation

30
Q

Reverse Thrust

A

Intentional selection of reverse thrust in​ flight is prohibited.

31
Q

Assumed Temp

A

Operation with​ assumed temperature reduced​ takeoff​ thrust is not permitted with​ ​anti-skid inoperative.

32
Q

APU Bleed (x 4)

A

Airplanes operating under FAA​ Rules:​

Inflight - APU bleed + electrical load: ​max​ alt 10,000ft.​
# Airplanes operating under FAA​ Rules:​ Ground only - APU bleed + electrical ​load: max alt​ 15,000ft.​
# APU​ bleed: max alt 17,000ft.​
# APU electrical load: max alt 41,000ft

33
Q

APU bleed valve must be closed when:

APU bleed​ valve may​ be open during engine start:

A

•​ ground​ air connected and isolation​ valve open​
•​ engine no. 1 bleed valve open​
•​ isolation and engine​ no. 2 bleed valves open

APU bleed​ valve may​ be open during engine start, but avoid​ engine power above ​idle.

34
Q

Aborted starts?

A

After three consecutive aborted start​ attempts, a fifteen​ minute cooling period​ is ​required

35
Q

APU run time before using it as a bleed source?

A

Run the APU for two​ full​ minutes before using it as​ a bleed air source

36
Q

Max Flap Alt

A

The maximum​ altitude with flaps extended​ is 20,000f

37
Q

Holding in Icing

A

Holding​ in icing conditions with flaps extended is prohibited

38
Q

Control Inputs

A

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

39
Q

Speed brakes

A

Do not​ deploy the speedbrakes in flight​ at radio​ altitudes less than 1,000ft

40
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 the alternate flap motor clutch​

After a complete extend/retract cycle,​ ie. 0 to 15 and​ back to 0, allow 5 ​minutes cooling​ before attempting another extension

41
Q

QFE ops?

A

QFE operations are prohibited

42
Q

GPWS (x2)

A

Do not use the terrain display for navigation.​

Do not use the look-ahead​ terrain alerting​ and terrain display functions:​
within​ 15nm of takeoff, approach or landing at​ an airport or runway not​ ​contained in the GPWS terrain​ database

43
Q

Wx Radar (x2)

A

Avoid​ weather radar operation in a hangar.​

Avoid​ weather radar operation when​ personnel are within the area normally ​enclosed by the airplane nose radome.​

Note:​ The hangar recommendation does not apply to the weather radar test mode

44
Q

Max and Min Fuel Temp?

A

Maximum​ tank fuel temperature is 49°C.​

Minimum tank​ fuel temperature prior to takeoff​ and inflight is - 43°C, or 3°C ​above the fuel freezing point temperature, whichever is higher.​

Note:​ The use of Fuel System Icing Inhibitor additives does not change the ​minimum​ fuel tank temperature limit

45
Q

Center Fuel Tank? (x2)

A

Intentional dry running of a center tank fuel​ pump (low pressure light illuminated) ​is prohibited.

Main tanks 1 and 2 must be full if center tank contains more than 453kg

46
Q

Fuel Balance?

A

Lateral imbalance between​ main tanks 1​ and 2 must be scheduled to be zero. ​Random fuel imbalance must​ not exceed 453kg for taxi, takeoff,​ flight or landing

47
Q

HGS (x2)

A

Use of HGS takeoff guidance as the sole means​ of runway centerline ​tracking​ is prohibited.​

The HGS is not approved​ for single engine fail​ passive rollout guidance. ​This does not prohibit​ use of the HGS rollout guidance as a ​supplemental aid during single engine operations.

48
Q

HGS Wind limits

A
49
Q

HGS Wind limits

A
50
Q

Brakes

A

Do not apply​ brakes until after touchdown

51
Q

Wingspan

A

35.79m
4C

52
Q

Min width pavement 180°turn?

A

24.3m

737 (1 decks)

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