Rotor blades - Study guides, Class notes & Summaries
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UH 60M CH8 Start Up/Shut Down
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Before Exterior Check Warning 
Do not preflight until armament systems are safe, switches off, safety pins in- stalled, and locking levers in locked position. 
 
 
 
When do you check for fuel sample? 
For contamination before first flight of the day 
For contamination after adequate settling time after cold refueling 
If the fuel source is suspected to be contaminated 
 
 
 
 
Nose Section Caution 
Do not deflect main rotor blade tips more than 6 inches below normal droop posi- tion when attach...
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Start Up and Shutdown test questions and answers
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8.18 before starting engines 
 
W W C 
W- main rotor blade tie-downs are removed 
 
W- While fully restrained at Design Eye Height, I must be able to manipulate all flight controls, propulsion, fuel, fire t-handles. 
 
C- Use hand hold for adjusting seats, not the foam glare shield 
 
 
 
8.19 COCKPIT EQUIPMENT CHECKS 
2.APU Control Switch - ON /// "APU-CLEAR" 
 
N N 
N- If APU ACCUM LOW does not appear, Pull manual override on accumulator manifold until APU reaches self-sustaining speed. 
 
N...
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Run-up/Shut-down exam questions with complete solutions.
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Before Starting Engines 
 
W W C 
 
W: All rotor tiedowns must be removed 
 
W: Make sure you have full flight control access/movement and can reach all the controls 
 
C: Don't grab the foam pad around the glare shield 
 
 
Parking break - release, then set 
Pressure applied, handle up, pressure released, handle released, parking break set 
 
 
 
0:01 
/ 
0:14 
Circuit breakers and switches - set 
 
N 
N: When expecting to go into IMC, hold STBY INST switch in TEST for 5 seconds and check for...
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Army Aviation Final Written Exam 2024.
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Army Aviation Final Written Exam 2024. 
 
the lift and thrust must exceed the weight and drag. increasing main rotor blades' AOA while maintaining their rotational speed creates extra lift and the aircraft ascends. 
Decreasing the pitch results in a descent. - correct answer vertical flight 
 
the increased efficiency of the rotor disk caused by interference of the airfloe when near the ground - correct answer in ground effect 
 
also known as dual rotor; has 2 large horizontal rotor assemblie...
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3B2 Power Engineer Exam Practice
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3B2 Power Engineer Exam Practice 
 
The disadvantages of a gas turbine are: 
1. High cost of manufacture 
2. High levels of noise pollution are produced 
3. Low thermal efficiency 
4. Requires many auxiliaries to be efficient 
 
A. 1, 2, 3 
B. 1, 3, 4 
C. 2, 3, 4 
D. 1, 2, 4 
E. 1, 2, 3, 4 - E 
 
The most common process method of refrigeration is: 
Select one: 
A. Absorption 
B. Lithium bromide 
C. Water vapor 
D. Vapor compression or mechanical 
E. Ammonia compression system - D 
 
To facilitat...
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army aviation questions with 100% correct answers graded A+ 2023
- Exam (elaborations) • 10 pages • 2023
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army aviationthe lift and thrust must exceed the weight and drag. increasing main rotor blades' AOA while maintaining their rotational speed creates extra lift and the aircraft ascends. 
Decreasing the pitch results in a descent. - correct answer vertical flight 
 
the increased efficiency of the rotor disk caused by interference of the airfloe when near the ground - correct answer in ground effect 
 
also known as dual rotor; has 2 large horizontal rotor assemblies instead of one main assembl...
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SIFT Study Guide || A + Verified Solutions.
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A helicopter is a type of...... correct answers Rotorcraft 
 
What are the three types of helicopters? correct answers single main rotor helicopters, tandem rotor helicopters, and coaxial rotor helicopters 
 
What is the most common design for a helicopter? correct answers single main rotor helicopter 
 
What is a disadvantage of the single main rotor helicopter? correct answers some power is used for countering torque, instead of just lifting 
 
What are some advantages of tandem rotor helicopt...
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ARMY Aviation Study Guide Test 2024.
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ARMY Aviation Study Guide Test 2024. 
the lift and thrust must exceed the weight and drag. increasing main rotor blades' AOA while maintaining their rotational speed creates extra lift and the aircraft ascends. 
Decreasing the pitch results in a descent. - correct answer vertical flight 
 
the increased efficiency of the rotor disk caused by interference of the airfloe when near the ground - correct answer in ground effect 
 
also known as dual rotor; has 2 large horizontal rotor assemblies in...
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TurboMachinery(Meng3201)Exit-ExamModule
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TurboMachinery(Meng3201)Exit-ExamModule 
 TsegayeGetachewAlenka 
 February19,2023 
 Contents 
 1 CourseObjectivesandCompetence 1 
 2 Introduction 1 
 2.1 TurbomachineryClassification. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 
 2.1.1 ClassificationCriteria . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 
 2.2 Application . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ....
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LSE school study guide || with 100% Errorless Answers.
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what are the primary missions of the UH-1? correct answers Utility, SAR, VIP, and Troop Transport 
 
what manual can every aircrafts tie-down points be found in? correct answers NA 00-80T-122 
 
specific aircraft, NATOPS 
 
what are Egress Points? correct answers any area of the helicopter from which an emergency EXIT/EGRESS can be safely made 
 
what is the primary method of starting a Cobra (AH-1) correct answers Two 24-VOLT NICAD Batteries 
 
what's some specific features of the Cobra? corre...
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