Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

B737-800 VXP > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Takeoff and Landing Tailwind Component

A

15 Knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Maximum Speeds

A

Observe Vmo Pointer and Gear/Flap Placecards

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Turbulent Airspeed

A

280 Konts / .76 Mach

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Minimum Runway Width

A

98 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Flight Deck Door Access System

A

Verify that an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Passenger Evacuation

A

Cabin occupants >1, all doors must be armed and verified prior to taxi, takeoff and landing.

0 Cabin occupants, forward doors only required to be armed and verified prior to taxi, takeoff and landing

(On flights with one or more occupants in the cabin, all entry door evacuation slides must be armed and engagement of the girt bar with door still verified prior to taxi, takeoff, or landing. On flights with no occupants in the cabin, only the two forward escape slide retention bars (girt bars) must be installed during taxi, takeoff, and landing.)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

HF Radios/Fueling

A

Do not operate HF Radios durning Refueling

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Flaps Certified for Takeoff

A

Flaps 1,5,10,15,25

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Cabin Altitude Briefing

A

As part of the takeoff briefing before engine start for the first flight of the day or following any change of either flight crew member, the PIC shall ensure the CABIN ALTITUDE WARNING indications and procedures are briefed in accordance with normal procedures of this manual. If a CABIN ALTITUDE WARNING LIGHT is installed, this briefing is not required.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Engine Anti-Ice System

A

Must be on:
All ground and flight operations when:
Icing conditions exist or are anticipated, except climb and cruise with SAT -40 deg C or greater.

Must be on prior to and during decent in icing conditions including temperatures below -40 deg C

(The engine anti-ice system must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when SAT is below -40 deg C. Engine anti-ice must be on prior to and durning decent in icing conditions, including temperatures below -40 deg C.)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Wing Anti-Ice System

A

Do not use wing anti-ice as a substitute for ground deicing/ anti-icing and inspection procedures that are necessary to comply with TEM deicing manual procedures. Do not operate wing anti-ice on the ground when the OAT is above 10 deg C (50 deg F)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Aileron Trim with Autopilot Engaged

A

Prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Autopilot takeoff engagement altitude

A

400 feet AGL or greater.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Single Channel Approach - Autopilot mandatory disengagement altitude

A

50 feet AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Do not use Level Change on final approach below what altitude

A

1000 feet AFE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Maximum takeoff EGT

A

950 deg C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Maximum Continuous EGT

A

925 deg C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Maximum Start EGT

A

725 deg C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Maximum Altitude for Flap Extension

A

20,000 feet pressure altitude

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

In flight, do not extend the speed brake lever beyond…

A

The flight detent

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

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….

A

VA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Holding in Icing conduction with Flaps extended

A

is PROIBITED

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Do not apply speed brakes in flight at flap settings greater then

A

Flaps 10

24
Q

Do not deploy speed brakes at radio altitude less than

A

1000 feet

25
Q

Flap 15 landings may be performed when required by a non-normal procedure. When is flaps 15 not authorized

A

Normal landings

26
Q

Vertical Situation Display

A

When installed, all non-ILS/ non-precision approaches, the PM must have the Vertical Situation Display (VSD) selected to on to enhance ground/ terrain situational awareness

27
Q

Fuel pump circuit breaker

A

Do not reset

28
Q

Maximum Fuel Temperature

A

49 deg C

29
Q

Minimum fuel temperature

A

Fuel freeze point of fuel being used +3 deg C or -43 deg C, whichever is higher (warmer)

30
Q

Operating Center Tank Pump on ground

A

Must not be positioned to ON unless center tank fuel quantity exceeds 1000 pounds, except when refueling or transferring fuel

31
Q

Center Tank Fuel Pumps must not be ON unless

A

Personel are available in the flight deck to monitor low pressure lights

32
Q

Center tank fuel pumps must be OFF when…

A

< 5000 pounds and when the aircraft is readied for initial taxi

<1000 pounds during climb

<3000 pounds durning decent and landing

33
Q

Operation with assumed temperature reduced takeoff thrust is no permitted with

A

Anti-Skip Inoperative

34
Q

Runway Slope

A

+/- 2%

35
Q

Maximum Flight Operating Latitude

A

82 deg North and 82 deg South

36
Q

Maximum Operating Altitude

A

41,000 feet

37
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet pressure altitude

38
Q

Flight Maneuvering Load Acceleration Limits

A

Flaps Up: +2.5g to -1.0g

Flaps Down: +2.0g to 0.0g

39
Q

B737 certificated in the Transport Category

A

14 CFR, Part 25 and Part 36

40
Q

B737 Kind of Airplane Operations

A

Both day and Night, when required equipment is installed and approved in accordance with the applicable FAR

VFR
IFR
Icing Conditions
Extended Over-water

41
Q

Flight Crew

A

Pilot and CoPilot

42
Q

Photoluminescence Floor Emergency Lighting System

A

PL Floor Emergency Lighting must be charged in accordance with approved procedures. Refer to AFM Supplements Chapter for Aircraft Specific Procedures.

43
Q

Brake Cooling

A

Observe minimum ground time shown on the Recommended Brake Cooling Schedule chart in the Performance Inflight section the QRH

44
Q

Maximum Taxi Weight

A

174,700 lbs

45
Q

Maximum Takeoff Weight

A

174,200 lbs

46
Q

Maximum Landing Weight

A

146,300 lbs

47
Q

Maximum Zero Fuel Weight

A

138,300 lbs

48
Q

Maximum Cabin Differential

A

9.10 psi

49
Q

Maximum allowable cabin differential pressure for takeoff and landing

A

0.125 psi

50
Q

Maximum Time Limit for Takeoff Thrust

A

5 Mins

51
Q

Maximum N1 RPM

A

104%

52
Q

Maximum N2 RPM

A

105%

53
Q

Minimum Oil Pressure

A

13 psi

54
Q

Maximum Fuel Temperature

A

49 deg C

55
Q

Fuel Tanks
No.1 and No.2

A

1288 gallons per tank

9144 lbs per tank

56
Q

Fuel tanks
Center

A

4081 Gallons

28,803 lbs

57
Q

Fuel Tanks

Total usable quantity

A

6,875 gallons

46,063 lbs

B737-800 VXP (2 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions