What is the maximum amount of baggage that can be carried when the airplane is loaded as follows front seat occupants 387 lb?
(Refer to figures 33 and 34.) What is the maximum amount of baggage that can be carried when the airplane is loaded as follows? A) 220 pounds. B) 45 pounds.
|Pilot and front passenger||310||—|
|Fuel, 38 gal||—||—|
What is the maximum amount of baggage that can be carried when the the airplane is loaded as follows?
(Refer to Figures 32 and 33) What is the maximum amount of baggage that can be carried when the airplane is loaded as follows? a. 45 pounds. (Refer to Figures 32 and 33) Calculate the weight and balance and determine if the CG and the weight of the airplane are within limits.
What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope view Figure 34?
79.2, normal category. (Refer to Figure 34.) What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope? 105 pounds.
Which action can adjust the airplanes weight to maximum gross weight and the CG within limits for takeoff?
Determine if the airplane weight and balance is within limits. A) 20 pounds overweight, CG forward of forward limits. B) 20 pounds overweight, CG aft of aft limits.
|Pilot and front passenger||250||—|
What is the maximum baggage that may be loaded for the CG to remain within the moment envelope?
What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope? 80.8, utility category. (Refer to Figure 34.) Calculate the moment of the airplane and determine which category is applicable.
How much does 8 quarts of aviation oil weigh?
Baggage 200 lb. Airplane B 1,200 pounds empty weight 8 quarts of oil (7.5 lb.
How many tons does a 737 weigh?
|Type||MTOW [kg]||MLW [tonnes]|
|Boeing 727-200 Advanced||84,000||70.1|
How is aircraft max payload calculated?
Subtract the basic empty weight and fuel from the maximum weight. Check the aircraft’s weight and balance sheet and find the maximum allowable gross weight of the aircraft. Then, find the basic empty weight value and subtract that from the max weight to get your “useful load” weight.
How does CG affect stability?
The aircraft becomes less stable as the CG is moved rearward. This is because when the CG is moved rearward it causes an increase in the AOA. … Any CG movement further aft results in an unstable aircraft. A forward CG location increases the need for greater back elevator pressure.
How much does airplane oil weigh?
Unless the specific weight for an item is known, the standard weights used in aircraft weight and balance are as follows: Aviation gasoline 6 lb/gal. Turbine fuel 6.7 lb/gal. Lubricating oil 7.5 lb/gal.
What effect does a 35 gallon fuel burn?
What effect does a 35-gallon fuel burn (main tanks) have on the weight and balance if the airplane weighed 2,890 pounds and the MOM/100 was 2,452 at takeoff? Correct answer: C. 210 pounds less and the aircraft is aft of the limits. First calculate the burn of fuel- 35 gallons at 6 pounds per gallon = 210 pounds less.
How should the 500 pound weight be shifted to balance?
How should the 500 pound weight be moved to balance the plank on the fulcrum? Answer: 500 lbs. (X) = 250 lbs.
What is the maximum gross weight of an airplane in the normal category?
(a) Certification in the normal category applies to airplanes with a passenger-seating configuration of 19 or less and a maximum certificated takeoff weight of 19,000 pounds or less.
How do airlines calculate weight and balance?
A: Many airlines use computer weight and balance programs. The airplane is divided into zones and the number of passengers in each zone is entered in the program. This allows for the balance of the airplane to be determined. It is likely that your flight was near a limit and they did not want people changing zones.
Does weight affect aircraft range?
As weight increases, the angle of attack for the best L/D ratio is at a higher IAS (thus TAS is higher), more speed means more drag and more power is required and it is out of proportion too because Power = Drag × TAS. Thus specific air range is lower with an increase of aircraft weight.