Limitations Flashcards
Max takeoff weight
351,000
Max taxi weight
352,200
Minimum Inflight Weight
168,000
Max Landing Weight
283,000
Max Zero Fuel Weight
266,000
If Landing Weight 272,000 lbs.or less
Wing fuel at landing must be 79,000 or Less
If Landing Weight Over 272,000 lbs.
Wing fuel at landing must be 43,000 or Less
• Runway Slope Limits:
±2%
Maximum Operating Altitude:
43,100 PA
Maximum Takeoff and Landing Altitude:
8,400 PA
Maximum Tailwind Component:
10kts
(Not considered limiting on a dry runway with all engines operating)
29 it’s
Turbulent Air Penetration:
290 kts IAS/.78M
MAX DIFF BETWEEN CAPTAIN OR FO AND FIELD ELEVATION
Sea level 75
5000 feet 75
10,000 feet 75
MAX DIFF BETWEEN CAPTAIN AND FIRST OFFICER
Sea Level 40 feet
5,000 feet 45 feet
10,000 feet 50 feet
MAIN CARGO DOOR
Maximum wind for door operation 40 knots. Maximum wind with door open (static) 60 knots.
AUTOFLIGHT
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.
Aircraft N1 Limit N2 Limits
B767-200 GE CF6-80A
117.0% 110.5%
AUTOLAND MAX WIND SPEEDS
Headwind 25 knots
Crosswind 25 knots
Tailwind 10 KNOTS
EGT LIMITS
ENGINE CF6-80A
Starting 750°C
Takeoff (5 Min) 940°C
Continuous 895°C
Minimum oil quantity for dispatch
17 QTS
Min oil pressure
10 psi
Max. Oil Temp.
160°C (Continuous Operation)
Max.Temp/Time
175°C for 15 min.