Limitations Flashcards

0
Q

Max takeoff weight

A

351,000

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1
Q

Max taxi weight

A

352,200

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2
Q

Minimum Inflight Weight

A

168,000

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3
Q

Max Landing Weight

A

283,000

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4
Q

Max Zero Fuel Weight

A

266,000

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5
Q

If Landing Weight 272,000 lbs.or less

A

Wing fuel at landing must be 79,000 or Less

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6
Q

If Landing Weight Over 272,000 lbs.

A

Wing fuel at landing must be 43,000 or Less

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7
Q

• Runway Slope Limits:

A

±2%

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8
Q

Maximum Operating Altitude:

A

43,100 PA

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9
Q

Maximum Takeoff and Landing Altitude:

A

8,400 PA

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10
Q

Maximum Tailwind Component:

A

10kts

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11
Q

(Not considered limiting on a dry runway with all engines operating)

A

29 it’s

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12
Q

Turbulent Air Penetration:

A

290 kts IAS/.78M

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13
Q

MAX DIFF BETWEEN CAPTAIN OR FO AND FIELD ELEVATION

A

Sea level 75
5000 feet 75
10,000 feet 75

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14
Q

MAX DIFF BETWEEN CAPTAIN AND FIRST OFFICER

A

Sea Level 40 feet
5,000 feet 45 feet
10,000 feet 50 feet

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15
Q

MAIN CARGO DOOR

A

Maximum wind for door operation 40 knots. Maximum wind with door open (static) 60 knots.

16
Q

AUTOFLIGHT

A

After takeoff, do not engage CMD mode below 400 ft.
Use of aileron trim with autopilot engaged is prohibited.

Autoland not authorized when aircraft weight exceeds max landing weight.

Amerijet policy does not allow use of autoland on CAT 1 runways except when performed for training purposes, with an authorized check airman.

17
Q

Aircraft N1 Limit N2 Limits

A

B767-200 GE CF6-80A

117.0% 110.5%

18
Q

AUTOLAND MAX WIND SPEEDS

A

Headwind 25 knots
Crosswind 25 knots
Tailwind 10 KNOTS

19
Q

EGT LIMITS

A

ENGINE CF6-80A
Starting 750°C
Takeoff (5 Min) 940°C
Continuous 895°C

20
Q

Minimum oil quantity for dispatch

A

17 QTS

21
Q

Min oil pressure

A

10 psi

22
Q

Max. Oil Temp.

A

160°C (Continuous Operation)

23
Q

Max.Temp/Time

A

175°C for 15 min.

24
Q

Maximum fuel temp Jet A

A

49° C

25
Q

Minimum fuel temp above freezing point

A

3° C

26
Q

Maximum fuel imbalance

A

2000 ± 500 lbs

27
Q

Maximum Flaps Altitude

A

20,000

28
Q

FLAP LIMIT SPEEDS (KTS)

A
1 / 240
5/ 220
15/210
20/195
25/190
30/162
29
Q

NAVIGATION

A

Do not operate IFR or at night into airports North of 73° N or south of 60° S Latitude whose navigational aids are referenced to magnetic north.

30
Q

AUXILIARY POWER UNIT

A

Do not use APU for pressurization above 17,000 feet.

31
Q

Engine Normal Duty Cycle

A

One (1) minute On, One (1) minute Off, Indefinitely

32
Q

Engine Extended Duty Cycle

A

1) Two (2) minutes ON, followed by One (1) minute OFF. 2) Five (5) minutes ON, followed by two and one half (2 1/2) minutes OFF. 3) Two (2) consecutive five (5) minute cycles require a ten (10) minute cooling period before additional five (5) minute cycles.

33
Q

Engine Re-engagement

A

0% N2 Recommended starter Re- engagement.

0-20% N2
Permissible starter Re- engagement.

21-30% N2

Permissible for purging or to clear a fire. Re- engagement above 30% N2 may result in starter or gearbox damage.
Note: A logbook entry is required whenever the starter is re-engaged above 20% N2.

34
Q

The starter duty cycle

A

a maximum of three consecutive starts or attempts within a sixty minute period with a 5 minute cooling period between attempts.