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767-200 AmeriJet Systems > General Limitations > Flashcards

General Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Max Operating Altitude

A

43100 PA

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3
Q

Max T/O and Landing Altitude

A

8400 PA

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4
Q

Max Tailwind

A

10 Kts

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5
Q

Max Crosswind

A

29 Kts

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6
Q

Turbulent Air Penetration

A

290 Kts/ .78M

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7
Q

Max Difference CPT/FO/Field Elevation (Altimeter)

A

75 Ft

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8
Q

Max Difference In Flight (RVSM)

A

200 FT

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9
Q

Max Difference CPT/FO @ S.L.

A

40 FT

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10
Q

Max Difference CPT/FO @ 5,000 FT

A

45 FT

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11
Q

Max Difference CPT/FO @ 10,000 FT

A

50 FT

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12
Q

Load Acceleration

Flaps UP

A

+2.5G to -1.0G

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13
Q

Load Acceleration

Flaps Down

A

+2.0G to 0G

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14
Q

Load Acceleration Note

Flap 25 and Flap 30

A

Limits vary linearly from +2.0G at Max Landing Weight to +1.5G at Max T/O Weight

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15
Q

Max Taxi Weight

A

352200

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16
Q

Max T/O Weight

A

351000

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17
Q

Min In-Flight Weight

A

168000

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18
Q

Max ZFW

A

266000

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19
Q

Max Landing Weight

A

283000

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20
Q

Landing Weight 272000 or LESS

A

W/F 79000 or less

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21
Q

Landing Weight Over 272000

A

W/F 43000 or less

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22
Q

Cargo Door Operation

A

40 Kts

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23
Q

Cargo Door Open

A

60 Kts

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24
Q

Min Alt to Engage CMD

A

400 FT

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25
Q

Min Alt for use of A/P

A

50 FT -MDA/ +AGL

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26
Q

Autoland

Max Headwind

A

25 Kts

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27
Q

Autoland

Max Crosswind

A

25 Kts

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28
Q

Autoland

Max Tailwind

A

10 Kts

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29
Q

Autoland Note

A

Not authorized if aircraft exceeds Max landing weight

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30
Q

N1

A

117.0%

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31
Q

N2

A

110.5%

32
Q

Starting EGT

A

750 C

33
Q

Take-off (5 min)

A

940 C

34
Q

Continuous

A

895 C

35
Q

Min Oil Pressure

A

10 PSI

36
Q

Max Oil Temp (Continuous Operation)

A

160 C

37
Q

Max Oil Temp/Time

A

175 C for 15 min

38
Q

Min Oil Quantity (Dispatch)

A

17 Quarts

39
Q

Engine Limits Note

A

Operate CONT Ignition in severe turbulence

DO NOT blank engine vibration display during T/O

40
Q

Navigation

Do not operate

A

IFR or Night of 73N or 60S

41
Q

VOR Approach

A

1 pilot must have VOR raw data

42
Q

TAAD Override selected when

A

IRS in NAV only mode, within 15nm of T/O, APP, or Landing.

When airport has no instrument approach or Runway less than 3500 Ft

43
Q

Max Fuel Temp

A

49 C

44
Q

Min Fuel Temp above Freezing

A

3 C

45
Q

Max Fuel Imbalance

A

2000 +/- 500

46
Q

Fuel Note

A

Use of JP-4 and Jet B fuels prohibited in revenue operations
Do not operate HF radios during refueling operations

47
Q

Fuel Loading
Center tank may contain ___________ of fuel with LESS than full main tanks, provided _____________________________________ dose not exceed ___________________________ limits are observed

A

22050 lbs , center tank fuel weight plus actual ZFW , MAX ZFW and CG

48
Q

Fuel usage (No Center Tank)

A

Use tank to engine for T/O and landing with all operable main tank fuel pumps on and X-feed valves closed
Open X-feed valves for min fuel operation or to correct fuel imbalance

49
Q

Fuel usage (Fuel in Center Tank)

A

..

50
Q

Max Fuel Imbalance (Chart)

A

…

51
Q

Max Flap Altitude

A

20000 FT

52
Q

Ice conditions exist On Ground

A

OAT 10 C or Below and visible moisture vis <1 mile

53
Q

Ice Conditions Exist In Flight

A

TAT 10 C or Below and visible moisture vis <1 mile

54
Q

Ice Note

A

Place Engine anti-ice on during all ground and flight operations when icing conditions exist or are anticipated EXCEPT below -40 C

DO NOT Use when Temp is above 10 C

55
Q

APU Starter Cycle

A

3 in 60 mins (5 min cooling in between)

56
Q

APU pressurization

A

17000 FT

57
Q

Powerplant Starter

Normal Duty Cycle

A

1 min on / 1 min off

58
Q

Powerplant Starter

ext. Duty Cycle

A

2 min on / 1 min off
5 min on / 2 1/2 min off
2 consecutive 5 min cycles require 10 min cooling before additional 5 min cycle

59
Q

Starter Re-engagement

0% N2

A

Recommend

60
Q

Starter Re-engagement

0-20% N2

A

Permissible

61
Q

Starter Re-engagement

21-30% N2

A

Purge/Fire only

LOG book entry required

62
Q

Flap 1

A

240 Kts

63
Q

Flap 5

A

220 Kts

64
Q

Flaps 15

A

210 Kts

65
Q

Flap 20

A

195 Kts

66
Q

Flap 25

A

190 Kts

67
Q

Flap 30

A

162 Kts

68
Q

Wing Span

A

156’ 1”

69
Q

Length

A

159’ 2”

70
Q

Tail

A

52’

71
Q

Fuselage width

A

16’ 6”

72
Q

Turn Radius

A

129’

73
Q

Main Fuel Tank

A

40700

74
Q

Center Fuel Tank

A

30500

75
Q

Total Fuel

A

111900

767-200 AmeriJet Systems (2 decks)

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