Maneuver Standards

Question 1

TASK 1040
Perform Visual Meteorological Conditions (VMC) Takeoff

Answer 1

1. Maintain takeoff heading ±10 degrees below 50 feet or until clear of the obstacles, or limited power takeoff until through ETL.
2. Maintain ground track alignment with the takeoff direction.
3. Maintain the aircraft in trim above 50 feet AGL or as appropriate for obstacle avoidance.
4. Accelerate to desired airspeed ±10 knots.
5. Apply takeoff power, not to exceed maximum available for the selected takeoff, until reaching desired altitude, minimum single engine airspeed, or as conditions permit

Question 2

TASK 1062
Perform Slope Operations

Answer 2

1. Set the parking brake/flight page prior to landing.
2. Maintain heading ±5 degrees.
3. Maintain minimum drift after wheel contact with the ground.
4. Do not exceed slope limits of the current operator’s manual.
5. Perform a smooth, controlled descent and touchdown.
6. Perform a smooth, controlled ascent

Question 3

TASK 1064
Perform a Roll-On Landing

Answer 3

1. Touchdown at or above ETL
2. Maintain ground track alignment with the landing direction with minimum drift.
3. Maintain a constant approach angle to the desired point of touchdown with deviations for surface conditions or obstacles in the landing area.
4. Maintain runway or suitable landing area alignment +/-5 degree

Question 4

TASK 1114
Perform Rolling Takeoff: Before liftoff

Answer 4

a. Position the stabilator to 0 degrees trailing edge down (TED).
b. Establish and maintain a simulated power limit of 10% below hover power ±3 % or, when IGE hover power is limited or not available, as described in the Task 1010 procedures ±3 %.
c. Coordinate accelerating the aircraft while maintaining aircraft longitudinal alignment in coincidence with the takeoff area’s heading/direction±5 degrees.
d. Do not allow the aircraft nose to drop below the fuselage level until the aircraft departs the takeoff surface

Question 5

standards: hover heading

Answer 5

±10 degeees

Question 6

standards: hover altitude IGE/OGe

Answer 6

2 feet
10 feet

Question 7

standards: hover drift IGE and OGE (80 ft)

Answer 7

3 feet IGE
12 feet OGE

Question 8

standards: hover ground track

Answer 8

3 feet

Question 9

standards: in flight heading

Answer 9

±10 degrees

Question 10

standards: in flight altitude

Answer 10

±100 feet

Question 11

standards: in flight airspeed

Answer 11

± 10 knots

Question 12

standards: in flight trim

Answer 12

± Ball

Question 13

Minimum safe altitude

Answer 13

Above the surface or obstacles to which the aircraft can descend in a masked condition

Question 14

Minimum maneuvering altitude

Answer 14

Altitude above the mask or barriers at which the aircraft may safely hover

Question 15

How can you determine OGE hover capability

Answer 15

Compare hover TQ OGE to max TQ available (dual engine) - If your predicted OGE Hover TQ is less than your Max TQ available then you have OGE Power.

Compare Max GWT OGE to current GWT - If your Take off gross weight is less than your max allowable gross weight then you have OGE Power.

Compare the predicted hover torque to the GO/NO GO torque OGE - If your predicted hover torque is less than your GO/NO GO torque OGE then you have OGE Power.

Question 16

Ground taxi TQ

Answer 16

25-30

Question 17

Standards: ground track for ground Taxi

Answer 17

± 3 feet

Question 18

Full scale deflection if velocity vector in hover mode is:

Answer 18

6 knots ground speed

Question 19

Full scale deflection if velocity vector in transition mode is:

Answer 19

60 knots

Question 20

Standards: VMC Takeoff

Answer 20

TQ 10% above hover
Heading 10 degrees Below 50 Ft
Above 50 ft in trim
Desired airspeed ± 10 knots (50 vx)

Question 21

Bingo fuel

Answer 21

Minimum fuel necessary to fly to a refuel site

Question 22

Joker fuel

Answer 22

The fuel point where training is terminated above bingo

Question 23

Buster

Answer 23

Max continuous speed (VH)

Question 24

Liner

Answer 24

Max range fuel

Question 25

Saunter

Answer 25

Best endurancr

Question 26

Standards: Slope operations heading

Answer 26

± 5

Question 27

Standards: slopes center cyclic with no less than-

Answer 27

25% TQ to avoid droop stop pounding

Question 28

Roll on landing aerodynamic braking

Answer 28

25% DE 50% SE

Question 29

Standards: roll on alignment

Answer 29

± 5 degrees

Question 30

Standards SE landing speed

Answer 30

Maintain speed at or above VSSE until 30 ft to the 1st 1/3 of the usable runway

Question 31

Standards: Autorotation call outs

Answer 31

Rotor Airspeed Trim

Question 32

Standards: Autorotation speed

Answer 32

No less than 70 knots prior to decel

Question 33

Standards: Rolling takeoff

Answer 33

Zero stab 10% below hover ± 5 Heading Nose can’t drop below fuselage lvl

Question 34

Continuous angle TO

Answer 34

Power: robust

Question 35

Altitude over airspeed take off Power Margin

Answer 35

Power: marginal oge

Question 36

Airspeed over altitude takeoff

Answer 36

Power: OGE pwr not available

Question 37

Low level flight

Answer 37

80-200ft

Question 38

Contour

Answer 38

25-80ft

Question 39

NOE

Answer 39

Up to 25ft

Question 40

When to abort a slope

Answer 40

Upslope landing gear slides Brakes don’t hold Cyclic stop encountered Comfort margin exceeded

Question 41

Standards: Limited power TO

Answer 41

Hover power available Cond not suitable for rolling TO Determine: ETL and abort point Speed: no less than VSDE ±5 Once through ETL, for acceleration a 5-degree nose low attitude is recommended. Avoid unnecessary accelerative attitudes of more than 10-degree nose low.

Question 42

VMC level accel

Answer 42

TQ 10% above hover Heading 10 degrees Below 50 Ft Above 50 ft in trim Speed min VSSE prior to climb This profile will aid the crew in establishing airspeed and reduce the risks associated with operation in the avoid region should an engine fail.

Question 43

Abort a slope

Answer 43

upslope landing gear begins to slide, aircraft brakes do not hold, a physical cyclic stop is encountered, crewmember's comfort margin is exceeded

Question 44

TASK 1082 Respond to Dual Engine Failure

Answer 44

1. Cruise-straight ahead or with a turn. a. Ensure the aircraft is in a position to make the desired landing location prior to descending below 200 ft. AGL. b. Visually check and call out NR, airspeed, and aircraft trim. c. Ensure that the airspeed is not less than E 70 KTAS prior to initiation of deceleration. d. Execute a deceleration no lower than 80 feet agl and termination 2. Terrain flight. Execute a deceleration and termination as directed by the IP

Question 45

TASK 1079 Respond to Engine Failure in cruise

Answer 45

SE failure in cruise flight. a. Recognize the emergency and perform the appropriate corrective actions. b. Adjust airspeed to remain within SE airspeed limits. c. Adjust airspeed to max RC/END (no single engine capability)

Question 46

TASK 1079 Respond to Engine Failure OGE or IGE

Answer 46

1. OGE. a. Recognize the emergency and perform the appropriate corrective action. b. Establish single engine flight with minimum loss of altitude or effect a smooth and controlled touchdown in a suitable area. c. Establish entry altitude, +50 feet, -0 feet. 2. IGE. Execute a smooth, controlled descent and touchdown with no lateral drift.

Question 47

TASK 1155 Negotiate Wire Obstacle

Answer 47

1) Over flight. Identify the top of the pole and the highest wire. Cross near a pole to aid in estimating the highest point. Minimize the time that the aircraft is unmasked. (2) Under flight. When under flying wires, maintain a minimum wire clearance of displayed hover height plus 30 feet. Compute minimum wire height by adding 30 feet to the hover height. This will give approximately a 12-foot clearance between the top of the aircraft and the wire (ground speed no greater than that of a brisk walk) (3) Ground taxi. Minimum wire height is 30 feet for ground taxi. When ground taxiing under wires, maintain a minimum wire height of 30 feet and ground taxi at a speed appropriate for the condition. During ground taxi only, this will result in approximately a 12-foot clearance poles.

Question 48

TASK 1114 Perform Rolling Takeoff

Answer 48

1. Before liftoff. a. Position the stabilator to 0 degrees trailing edge down (TED). b. Establish and maintain a simulated power limit of 10% below hover power ±3 % or, when IGE hover power is limited or not available, as described in the Task 1010 procedures ±3 %. c. Coordinate accelerating the aircraft while maintaining aircraft longitudinal alignment in coincidence with the takeoff area's heading/direction±5 degrees. d. Do not allow the aircraft nose to drop below the fuselage level until the aircraft departs the takeoff surface. 2. After liftoff. a. Maintain a simulated power limit of 10% ±3 below hover power or, when IGE hover power is not available, as described in the Task 1010 procedures ±3 %. b. Maintain takeoff ground track. c. Establish the aircraft in trim commensurate with obstacles. d. Establish and maintain a climb angle appropriate for the terrain and obstacles. e. Accelerate to maximum R/C or desired airspeed

Question 49

TASK 1058 Perform Visual Meteorological (VMC) Conditions Approach

Answer 49

1. Select a suitable landing area. 2. Evaluate power required versus power available for the type of approach selected. 3. Maintain a constant approach angle to the desired point of termination (hover or touchdown) with deviations for surface conditions or obstacles at the point of termination. 4. Maintain ground track alignment with the landing direction with minimum drift. 5. Maintain rate of closure appropriate for the conditions. 6. Align aircraft with landing direction below 50 feet or as appropriate for obstacle avoidance. 7. Perform a smooth and controlled termination to a hover or to the ground at the intended point of touchdown.

Question 50

OGE power NA

Answer 50

Masking Unmaskimg ITO NOE Terrain flight TO (alt/as) Respond to engine failure VMC approach to OGE hover

Question 51

Common standards for all maneuvers

Answer 51

Do not exceed aircraft limitations. Perform crew coordination actions IAW aircrew coordination section in this ATM. Utilize applicable terminology IAW ATP 1-02.1

Question 52

TASK 1082 Respond to Dual Engine Failure

Answer 52

Rotor airspeed trim prior to 200 ft agl Decel prior to 80 feet

Question 53

3 types of terrain flight take offs

Answer 53

Continuous angle Airspeed over altitude Altitude over airspeed

Question 54

When do you terminate your takeoff?

Answer 54

Clear obstacles Desired airspeed Positive rate of climb

Question 55

CMF

Answer 55

Deceleration turn Break turn Cyclic climb to pushover break Pitch back turn Dive recovery

Question 56

TASK 1127 Perform Basic Maneuvering Flight

Answer 56

Transient torque Rotor coming Weight lift correlation Airspeed altitude trade off Pitch down tendency

Question 57

Why would you perform a roll on landing? (With DE capability)

Answer 57

IGE power is not available; for example, high DA or GWT The low airspeed indicator and the “Airspeed Low” voice (VSDE) DVE

Question 58

When do you need to conduct a OGE power check?

Answer 58

If the margin between OGE power required and MAX TRQ AVAIL is marginal (

Question 59

Task 1182

Answer 59

Attitude Torque Altitude Heading Airspeed

Question 60

TASK 1182 Perform Unusual Attitude Recovery/ Respond to Spatial Disorientation

Answer 60

Phase-1, Regain basic control: (A) ATTITUDE-Level the pitch and bank attitude while maintaining the aircraft in trim. (T) TORQUE-Adjust collective/thrust as required. (A) ALTITUDE-Adjust to desired altitude after establishing initial aircraft control. Phase-2, Stabilize: (H) HEADING-Establish and maintain heading, turn only to avoid known obstacles. (A) AIRSPEED-Adjust airspeed as necessary