Limitations Flashcards

1
Q

Runway slope

A

+/- 2%

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2
Q

Maximum takeoff and landing tailwinds component

A

10 knots
(A series G series,BXI, BXJ 15 knots FAA approved This finding​ does not constitute ​operational approval to conduct takeoffs ​or landings with tailwind components ​greater than 10 knots.)

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3
Q

Maximum​ Operating Altitude​

A

41000 ft

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4
Q

Maximum​ Takeoff and Landing Altitude​

A

8,400 feet​ pressure altitude

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5
Q

ONLY B737 MAX
Ground​ Wind​ Operating Envelope​

A

•​ For crosswinds greater than​ 43 knots, limit​ thrust​ to a setting​ normally​ ​used for taxi.​
•​ Except when setting​ takeoff thrust on​ the runway, limit engine thrust to ​idle for winds greater than 58 knots.

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6
Q

Severe Turbulent Air Penetration speed

A

280 KIAS / .76M
whichever is lower.​ ​Applicable to Climb and Descent​ only
For cruise use supplementary procedures

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7
Q

Non–AFM​ Operational Information
Refueling
Revenue flights

A

Do not operate HF radios during refueling​ operations.

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

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8
Q

Altitude Display Limits​ for​ RVSM Operations

A

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

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9
Q

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

A

200 feet

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10
Q

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

A

Difference between capt and FO upto 5000ft 50 feet

Difference between capt and FO Above 5000 upto 10000 60 feet

Difference between crew and field elevation 75 feet

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11
Q

Possible conflicts between the AFM and the FCOM

A

conflict between the ​FCOM and the AFM, the AFM shall govern

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12
Q

737NG Weight Limitations Taxi, takeoff, landing, zero fuel.

A

Maximum Taxi Weight​ 79,242 Kilograms

Maximum Takeoff Weight​ 79,015 Kilograms

Maximum Landing Weight​ 66,360 Kilograms

Maximum Zero Fuel Weight​ 62,731 Kilograms

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13
Q

737 MAX Weight Limitations Taxi, takeoff, landing, zero fuel.

A

Maximum Taxi Weight​ 82,871 Kilograms

Maximum Takeoff Weight​ 82,644 Kilograms​

Maximum Landing Weight​ 69,308 Kilograms

Maximum Zero Fuel Weight​ 65,952 Kilograms

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14
Q

The maximum cabin differential pressure (relief valves) is

A

9.1 psi

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15
Q

the air ​conditioning packs in HIGH With either one or both​ engine bleed air switches ON

A

DO NOT operate the air ​conditioning packs in HIGH for takeoff, approach or landing.( does not apply for NON NORMALS)

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16
Q

@Boeing 737NG Auto Pilot

A

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

# Do not use LVL​ CHG on final approach below 1000​ feet AFE
# Do not​ engage the autopilot for takeoff below 400 feet AGL.​
FAA​ Rules:​
# For single channel operation during approach, the autopilot shall not remain ​engaged below 50​ feet​ AGL

17
Q

@Boeing 737 MAX Auto Pilot

A

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

# Do not​ engage the autopilot for takeoff below 400 feet AGL.
# Airplanes operating with EASA​ Certification: The Minimum Use Height ​(MUH) for single channel​ autopilot​ operation is defined as 111 feet AGL
# Do not use LVL​ CHG on final approach below 1000​ feet AFE

18
Q

B737NG EDTO

A

One engine diversion speed-0.79M/330KIAS
Distance: 431 NM for 60 mins and 842NM for 120 mins
Threshold time: 60 mins
Max diversion time: 120 mins
Area of operations: ASIA,MID, EUR, AFRICA.