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767-200 AmeriJet Systems > General Limitations > Flashcards

General Limitations Flashcards

(75 cards)

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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
Min Alt for use of A/P
50 FT -MDA/ +AGL
26
Autoland | Max Headwind
25 Kts
27
Autoland | Max Crosswind
25 Kts
28
Autoland | Max Tailwind
10 Kts
29
Autoland Note
Not authorized if aircraft exceeds Max landing weight
30
N1
117.0%
31
N2
110.5%
32
Starting EGT
750 C
33
Take-off (5 min)
940 C
34
Continuous
895 C
35
Min Oil Pressure
10 PSI
36
Max Oil Temp (Continuous Operation)
160 C
37
Max Oil Temp/Time
175 C for 15 min
38
Min Oil Quantity (Dispatch)
17 Quarts
39
Engine Limits Note
Operate CONT Ignition in severe turbulence | DO NOT blank engine vibration display during T/O
40
Navigation | Do not operate
IFR or Night of 73N or 60S
41
VOR Approach
1 pilot must have VOR raw data
42
TAAD Override selected when
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
Max Fuel Temp
49 C
44
Min Fuel Temp above Freezing
3 C
45
Max Fuel Imbalance
2000 +/- 500
46
Fuel Note
Use of JP-4 and Jet B fuels prohibited in revenue operations Do not operate HF radios during refueling operations
47
Fuel Loading Center tank may contain ___________ of fuel with LESS than full main tanks, provided _____________________________________ dose not exceed ___________________________ limits are observed
22050 lbs , center tank fuel weight plus actual ZFW , MAX ZFW and CG
48
Fuel usage (No Center Tank)
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
Fuel usage (Fuel in Center Tank)
..
50
Max Fuel Imbalance (Chart)
...
51
Max Flap Altitude
20000 FT
52
Ice conditions exist On Ground
OAT 10 C or Below and visible moisture vis <1 mile
53
Ice Conditions Exist In Flight
TAT 10 C or Below and visible moisture vis <1 mile
54
Ice Note
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
APU Starter Cycle
3 in 60 mins (5 min cooling in between)
56
APU pressurization
17000 FT
57
Powerplant Starter | Normal Duty Cycle
1 min on / 1 min off
58
Powerplant Starter | ext. Duty Cycle
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
Starter Re-engagement | 0% N2
Recommend
60
Starter Re-engagement | 0-20% N2
Permissible
61
Starter Re-engagement | 21-30% N2
Purge/Fire only | LOG book entry required
62
Flap 1
240 Kts
63
Flap 5
220 Kts
64
Flaps 15
210 Kts
65
Flap 20
195 Kts
66
Flap 25
190 Kts
67
Flap 30
162 Kts
68
Wing Span
156' 1"
69
Length
159' 2"
70
Tail
52'
71
Fuselage width
16' 6"
72
Turn Radius
129'
73
Main Fuel Tank
40700
74
Center Fuel Tank
30500
75
Total Fuel
111900

767-200 AmeriJet Systems (2 decks)

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