Systems - introduction Flashcards
The UH-60M civilian model designation:
Sikorsky, S-70
UH-60M engines:
- 2 General Electric model T700-GE-701D series turbo shaft engines
- Approx. 2000hp each
The main rotor is _______ (Rigid/Semi Rigid/Fully Articulated)
Fully Articulated
Can you retract the landing gear?
No
The three parts the console is divided into:
(1) Overhead console
(2) Center Instrument Panel
(3) Lower Console
What is the Minimum Crew Requirements?
Minimum: Pilot and copilot: additional crewmembers, as required, will be added at the discretion of the commander, in accordance with pertinent Department of the Army regulations.
What is the normal Crew Requirements?
- Pilot right side of cockpit.
- Copilot left side of cockpit.
- Crew chief right forward side of cabin.
- Gunner left forward side of cabin
What is the primary mission of the UH-60m
Primary missions of this helicopter are tactical transport of troops, medical evacuation and cargo transport.
Basic weight:
Approx. 13.000 lbs
Design weight:
16.825 lbs
Max gross weight:
22.000
Rotor Diameter:
53 feet 8 inches
Rotor clearance Turning:
9 feet 5 inches
Rotor clearance Sloping:
7 feet 7 inches
WARNING: Main rotor clearance is shown with cyclic _____ and _____. Cyclic _____ or _____ may cause rotor blade clearance to be significantly less
WARNING: Main rotor clearance is shown with cyclic centered and level ground. Cyclic displacement or sloping terrain may cause rotor blade clearance to be significantly less
Tail rotor is canted at _____ degrees to improve performance and increase lift capability. The _____ degree cant provides approximately _____ of the total lifting force for the aircraft.
Tail rotor is canted at 20 degrees to improve performance and increase lift capability. The 20 degree cant provides approximately 2.5% of the total lifting force for the aircraft.
Stabilator width:
14 feet 4 inches
When ground taxing, the UH-60 requires _____ feet _____ inches of tail rotor clearance for a 180 degree turn
When ground taxing, the UH-60 requires 41 feet 7.7 inches of tail rotor clearance for a 180 degree turn
Fuel Load consists of
Two interchangeable, crashworthy, ballistic-resistant fuel tanks are mounted on each side of the transition section.
Main tank usable fuel is _____ U.S. gallons, _____ per tank when gravity refueled, providing approximately _____ hours of flight time
Main tank usable fuel is 360 U.S. gallons, 180 per tank when gravity refueled, providing approximately 2.3 hours of flight time
The primary structure is _____ . Some _____ and _____ are used for firewalls and various fittings.
The primary structure is aluminum alloy. Some titanium and steel are used for firewalls and various fittings.
Aluminum paneling is used for added E3 protection. Where aluminum paneling couldn’t be used, _____ was used ?
Alluminum Mesh
Where does the Pre-Flight checks begin?
At the front of the helicopter
CAUTION: Do not deflect main rotor blade tips more than _____ below normal droop position when attaching tiedowns. Do not tie down below normal droop position.
CAUTION: Do not deflect main rotor blade tips more than 6 inches below normal droop position when attaching tiedowns. Do not tie down below normal droop position.
The rotor blade is designed with a _____ degree static twist, and the blade tip has a _____ degree sweep
The blade tip also has a _____ degree anhedral angle
The UH-60M is equipped with a wide chord (_____ inch) rotor blade with a _____ foot _____ inch span.
The rotor blade is designed with a 16.3 degree static twist, and the blade tip has a 30 degree sweep
The blade tip also has a 20 degree anhedral angle
The UH-60M is equipped with a wide chord (24.25 inch) rotor blade with a 24 foot 4 inch span.
In the front avionics compartment you’ll find
- Two aircraft Sealed Lead Acid Batteries (SLAB)
- Two Embedded Global Positioning/Inertial Navigation systems (EGIs)
- The #2 Flight Control Computer (FCC).
- Electric Standby Instrument System (ESIS) battery. PUSH TO TEST button