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Boeing 737NG > Limitations > Flashcards

Limitations Flashcards

0
Q

Maximum Tailwind

A

Option 10 kts
or
Option 15 kts

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1
Q

Runway Slope Limits

A

+/- 2%

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2
Q

Maximum Demonstrated Crosswind

A

36 kts without winglets

33 kts with winglets

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3
Q

Maximum Speed (Vmo/Mmo)

A

320 kias

0.82 m

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4
Q

Turbulent Air Penetration Speed

A

280 kias / .76m

250 kias when below 15,000 ft and below MLW

(AOM Vol. 1 SP.16.21)

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5
Q

Maximum Altitude

A

41,000 ft

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6
Q

Maximum Takeoff and Landing Altitude

A

8,400 ft
or
12,000 ft with Hight Altitude Option

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7
Q

Maximum Ramp Weight

A

156,000 lbs
or
174,700 lbs with IGW Option

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8
Q

Maximum Takeoff Weight

A

155,500 lbs

174,200 lbs with IGW option

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9
Q

Maximum Landing Weight

A

144,000 lbs

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10
Q

Maximum Zero Fuel Weight

A

136,000 lbs

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11
Q

Maximum Cabin Differential Pressure

A

9.1 psi

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12
Q

Maximum Altitude for APU Bleed and Electrical use

A

10,000 ft

*Under Captain’s Emergency Authority, APU has demonstrated the capability to supply both bleed air and electrical power up to 20,000 ft.

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13
Q

Maximum Altitude for APU Bleed Only Use.

A

17,000 ft

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14
Q

Maximum Altitude for APU Bleed and Electrical Use on Ground

A

15,000 ft

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15
Q

Maximum Altitude For APU Electrical Use Only

A

41,000 ft

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16
Q

Minimum Altitude for Autopilot use After Takeoff

A

400 ft AGL

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17
Q

Minimum Altitude for Autopilot “ON” During Non-Precision Approach

A

50 ft Below Minimums

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18
Q

Maximum Engine Limits

A

Redline

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19
Q

Minimum Engine Limits

A

Redline

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20
Q

Engine Caution Limits

A

Amber

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21
Q 
Engine Ignition Must Be On For:
\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_ \_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_
A

Takeoff
Landing
Heavy Rain
Anti-Ice

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22
Q

Maximum Flaps Extension Altitude

A

20,000 ft

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23
Q

Minimum Altitude For Speed Brake Use.

A

1,000 ft

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24
Q

Alternate Flap Duty Cycle (down and back up)

A

0-15-0 = 5 min.

> 15 = 25 min.

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25
Q

Fuel System Minimum Temperatures

A

-43˚C or 3˚C above fuel freezing

Whichever is warmer

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26
Q

Fuel System Maximum Temperatures

A

49˚C

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27
Q

Random Fuel Imbalance

A

1,000 lbs for Taxi, Takeoff, Landing

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28
Q

Icing Condition Temperature

A

10˚C/50˚F or below

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29
Q

Air Data Inertial Reference Unit (ADIRU) Alignment Must Not be Attempted at Latitudes Greater Than

A

78˚ 15 min

30
Q

Maximum Flight Operating Latitude

A

82˚ North and South (without Polar Navigation Option)

Exceptions:

Between 80˚W and 130˚W = 70˚N
Between 120˚E and 160˚E = 60˚S

31
Q

Photoluminescent Floor Lighting Must be ___________

A

Charged IAW Approved Procedures and Charging Table in AOM Chapter 1 section 40.

32
Q

Flight Deck Door Operational Check Must be Checked

A

Once a Day

33
Q

Escape Slide Retention Bar

A

Must be installed for Taxi, Takeoff, and Landing

34
Q

Standby Altimeter for RVSM Accuracy

A

Does not meet Accuracy Requirements for RVSM

35
Q

Maximum Altitude Difference Between Captain’s and FO’s Altimeters for RVSM Use While in Flight

A

200 ft

36
Q

Maximum Difference Between the Captain’s and FO’s Altimeters on the Ground for RVSM Use

A

Airport Elevation S.L. to 5000 ft = 50 ft

5001 ft to 10,000 = 60 ft

37
Q

Maximum Difference of Captain’s and FO’s Altimeters to Airport Field Elevation While on Ground

A

75 ft

38
Q

With Engine Bleed on do Not Run A/C Packs in _______ for Takeoff, Approach, or Landing

A

High

Note: Except for NNP (like Cargo Fire, Smoke Removal) Checklist Has Prioity.

39
Q

Engine TAI Must Be On When _______

A

In Icing Conditions or Icing Conditions are Expected.

Exception: During Climb and Cruise When Temp is Below -40˚C SAT

40
Q

De-Icing with Type II and IV fluids for Airplanes without Stiffened Elevator Tabs.

A

Max Speed 270 kias until Maintenance Procedures are Accomplished

41
Q

Autopilot Single Channel Approach Minimum Disengagement Altitude

A

50 ft AGL

RA 100 ft for airports above 8,400 ft onairplanes with Hight Altitude Option

42
Q

Maximum allowable wind components for Autoland Operations

Headwind: _________
Crosswind: _________
Tailwind: __________

A

25 kts
20 kts
15 kts

43
Q

Maximum allowable wind components for Autoland Operations (Cat IIIB)

Crosswind:______
Tailwind:_______

A 
25 kts (?)
10 kts
44
Q

Maximum and Minimum Glideslope Angles for Autoland

A

3.25˚ and 2.5˚

45
Q

Single Engine Cat IIIB Autoland Operations

A

Flaps 30 and only for DH at or above 50 ft AGL

46
Q

Maximum Pressure Altitude for use of Autoland

A

8,400 ft

47
Q

Integrated Approach Navigation (IAN)

A

Do not use if altitude constraints between the FAF and the runway have been modified by the flight crew.

48
Q

HUD System Maximum Latitude and Limit of use

A

85˚ Latitude or when heading reference is set to TRUE

with HGS 2350 and polar Nav

49
Q

Flight Dynamics Model 4000 Phase I HGS (HUD)

A

AIII Mode Approach and Landing not approved

50
Q

Limitation for use of VHF-3 for voice communications

A

Do Not Use with ACARS Operational

51
Q

ACARS Limitation

A

Limited to transmissions that will not creat an unsafe condition
Parts of messages delayed or not received
message delivered to wrong recipient
Correct message content

52
Q

Use of ACARS for clearances

A

Predeparture Clearance, D-ATIS, Ocianic Clearance, W&B, Takeoff Data messages may be used if from a verified and pre approved ops procedures.

53
Q

Use of VHF communications with ATC on the ground

A

Use Radio That is Connected to Top Antenna

54
Q

Use of auxiliary power outlets in the flight deck

A

Requires regulatory approval

55
Q

Reverse Thrust Limitation

A

Intentional use inflight is prohibited

56
Q

APU Bleed Valve Must Be Closed When

A

a - Ground Air is Connected and Isolation Valve is Open
b - Eng. #1 Bleed Valve is Open
c - Isolation Valve and Eng. #2 Bleed Valve is Open

57
Q

APU Bleed Valve May Be Open During Engine Start But:

A

Avoid Power Settings Above Idle.

58
Q

Holding In Icing Conditions With Flaps Extended

A

Prohibited

59
Q

Do Not Extend Speed Brake Lever Beyond _____ ______ When InFlight

A

Flight Detent

60
Q

Maximum Speed for Use of Speed Brakes

A

300 kias (for airplanes without stiffened elevator tabs)

use of speed brakes at speeds in excess of 320 kias can cause sever vibration and damage the horizontal stabilizer

61
Q

Rapid and Large Alternating Control Inputs

A

Avoid - May Result in Structural Failure Even Below Va

62
Q

Time Between Actuations of The Alternate Flap Switch

A

15 Seconds - avoids damage to motor’s clutch

63
Q

When QFE is Selected, Use of VNAV, LNAV, and Veridical Situation Display is _______

A

Prohibited

64
Q

Selection of QFE is Prohibited if _______

A

QFE Option Is Not Installed In The FMS

65
Q

Regarding the PFD, If QFE is Used Instead of QNH: _____________

A

Selection of QFE Must be Made in the FMS

66
Q

Use of Look Ahead Terrain Alerting:
a - Without GPS or
b - With GPS and an Older GPWS Computer

A

Is Prohibited

67
Q

Limitation On Use of Look Ahead Terrain Alerting (GPWS)
A - ____________________
B - ____________________

A

A - Do Not Use Terrain Display For Navigation
B - Do Not Use Within 15 min. of Takeoff, Approach, or Landing at
airports contained in the GPWS Database

68
Q

Use of Integrated Approach Navigation (IAN) With QFE is _______

A

Prohibited

69
Q

Weather Radar Limitations

A

Do Not Operate In a Hangar, 50ft From Personnel and Fuel Spills.

*Hangar and Personnel do not apply with radar in test mode.

70
Q

Scheduled Fuel Imbalance

A

0 (Zero)

71
Q

Main Fuel Tanks Must Be Full If ___________

A

Center Tank has More Than 1,000 lbs In It

72
Q

Anti-Skid INOP

A

Assumed Temperature Reduced Thrust Takeoff Is Not Permitted.

73
Q

Brakes

A

Do Not Apply Until After Touchdown

Boeing 737NG (5 decks)

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