Bell 407 | UPDATED Questions with 100% Verified Answers
Question:
Maximum Continuous Power
Answer:
93.5 % TQ
630 shp MC
Question:
Take off Power 5'
Answer:
93.5 to 100 % TQ
674 shp 5'
Question:
Vne
Answer:
140 Knts
Question:
Max Airspeed Autorotation
Answer:
100 Knts
Question:
Maximum Air speed at 93.5 % TQ
Answer:
100 Knts
Question:
Maximum airspeed with door off
Answer:
Any combination removed 100 Knts
,Question:
When Takeoff loading is in shaded area of the gross weight
lateral CG limits
Answer:
100 Knts
Question:
Minimum rate of descent autorotation
Answer:
55 Knts
Question:
Maximum glide distance autorotation
Answer:
80 Knts
Question:
Hydraulic Failure
Answer:
70 to 100 Knts
Question:
Best rate of climb
Answer:
60 Knts
Question:
Maximum operating altitude
Answer:
20,000' HP
Question:
,Maximum Altitude for takeoff, landing and ground affect
maneuvers
Answer:
11,000' HD
Question:
Maximum gross weight
Answer:
5,250 pounds
Question:
Maximum gross weight external
Answer:
6,000 pounds
Question:
Fuel, maximum capacity
Answer:
130 Galons 869 pounds
Question:
Fuel System
Answer:
Usable capacity 127 gallons 863 pounds
Question:
Fuel Pressure
Answer:
8 psi Minimum
8 to 25 Continuous operation
25 psi Maximum
Question:
, Engine oil
Answer:
6 U.S. Quarts
Question:
Transmission
Answer:
5 U.S. Quarts
Question:
Tail rotor gear box
Answer:
0.33 U.S. Quarts
Question:
Hidraulic System reservorio
Answer:
1.68 U.S. Quarts
Question:
Main Rotor is
Answer:
Four blade Soft in plane, flex beam tipe hub
Question:
Main Rotor
Answer:
4 blade, diameter 35 feet = 10.7 meters
Question:
Vx
Answer:
55 Knots Minimum
Question:
Maximum Continuous Power
Answer:
93.5 % TQ
630 shp MC
Question:
Take off Power 5'
Answer:
93.5 to 100 % TQ
674 shp 5'
Question:
Vne
Answer:
140 Knts
Question:
Max Airspeed Autorotation
Answer:
100 Knts
Question:
Maximum Air speed at 93.5 % TQ
Answer:
100 Knts
Question:
Maximum airspeed with door off
Answer:
Any combination removed 100 Knts
,Question:
When Takeoff loading is in shaded area of the gross weight
lateral CG limits
Answer:
100 Knts
Question:
Minimum rate of descent autorotation
Answer:
55 Knts
Question:
Maximum glide distance autorotation
Answer:
80 Knts
Question:
Hydraulic Failure
Answer:
70 to 100 Knts
Question:
Best rate of climb
Answer:
60 Knts
Question:
Maximum operating altitude
Answer:
20,000' HP
Question:
,Maximum Altitude for takeoff, landing and ground affect
maneuvers
Answer:
11,000' HD
Question:
Maximum gross weight
Answer:
5,250 pounds
Question:
Maximum gross weight external
Answer:
6,000 pounds
Question:
Fuel, maximum capacity
Answer:
130 Galons 869 pounds
Question:
Fuel System
Answer:
Usable capacity 127 gallons 863 pounds
Question:
Fuel Pressure
Answer:
8 psi Minimum
8 to 25 Continuous operation
25 psi Maximum
Question:
, Engine oil
Answer:
6 U.S. Quarts
Question:
Transmission
Answer:
5 U.S. Quarts
Question:
Tail rotor gear box
Answer:
0.33 U.S. Quarts
Question:
Hidraulic System reservorio
Answer:
1.68 U.S. Quarts
Question:
Main Rotor is
Answer:
Four blade Soft in plane, flex beam tipe hub
Question:
Main Rotor
Answer:
4 blade, diameter 35 feet = 10.7 meters
Question:
Vx
Answer:
55 Knots Minimum