Manuevers

Question 1

Initial Hover Checks

Answer 1

Brief CPG for pylon articulation
5' hover
Controllability / Stability
Vibrations / Stab full down + up / reset 
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Symbology / Radar altimeter check
Power check (CPG)
TSD UTIL (CPG)

Question 2

Hover Maneuvering Checks

Answer 2

5’-10’
90 deg right + left (CRIS)
Forward, lateral, and rearward flight (10’-15’)

Question 3

FMC ATT HOLD Checks

Answer 3

Reset SAS
5’-10’
ATT hold (symbology FLT page, HDU, + EUFD)
Disengage - note tone, symbology, and EUFD
ALT hold (symbology FLT page, HDU, + EUFD)
Disengage - note tone, symbology, and EUFD
______________________________
Engage ATT + ALT hold
Brief forced landing plan, OGE power + Settling with power (80’ or highest ob)
15% -20% above hover TQ
Note ALT disengages, tone, heading +/-5
Return to 5’ hover - engage ALT hold
_______________________________
Cyclic 1/2” in any direction
Note TRC symbology / return to trimmed position
Disengage holds via 6’o clock

Question 4

Visonic check

Answer 4

ALT hold
CPG video (pick target 500m away)
TADS DAY/FLIR N FOV
90 deg turns about the nose

Question 5

Hover Drift Box Check

Answer 5

EGIs keyed / 4 Satellites
ATT + ALT hold
Drop box (5m drift)

Question 6

Initial Take Off Checks

Answer 6

ENG / ENG SYS page
Control positions and response
30-40 Stab programming
Vibrations / Instruments
TQ within 5%

Question 7

Cruise Checks

Answer 7

Straight/Level 120 KTAS
Vibrations + Fuel consumption
Note TQ

Question 8

Autorotation

Answer 8

Transfer Controls - 90 KTAS start climb 1000' above record
Reset Altimeter to 29.92
Note PA, FAT, and GW - PERF page
Brief WCN, Before Landing Check, Target Nr
TQ less than 54% or half SE MAX TQ
PL - IDLE (Np/Nr split - Ng stable)
Select suitable landing area
Reduce collective (AS, Nr, Trim)
Rotor Stable
PL IDLE (Np/Nr split - Ng Stable)
Record Nr
PLs - Tach match
COL - 1 inch check
PLs - FLY
COL - Cruise TQ (forward cyclic)
Reset altimeter / verify record Nr

Question 9

Attitude Hold Check

Answer 9

120 KTAS
FLT + UTIL page
Brief CPG to verify FMC axes
ATT HOLD - symbology + EUFD
ALT HOLD - symbology + EUFD
FMC - release button (CPG verify axes disengaged + tone) less stable but controllable.
Master Caution reset - Note tone
CPG engage axes
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Left and right 20 deg turn (1/2 trim ball + Symbology)

Question 10

Maneuvering Flight

Answer 10

120 KTAS - Note vibrations
20% torque / 120 KTAS vibrations, control placement, stability
MAX CON TQ / 120 KTAS vibrations, control placement, stability

Question 11

Stabilator Check

Answer 11

ENG + ENG SYS page
Brief CPG to select NOE/APP mode
Slow to less than 80 KTAS maintain ALT
Note Stab 25 deg down
Increase airspeed above 80 KTAS maintain ALT
Reset Stab on COL (verify disengaged)

Question 12

Vh Check

Answer 12

Increase COL to MAX CON TQ or limit / maintain ALT
Vibrations / Control / Max travel
Note TGT

Question 13

ETF Check

Answer 13

Transfer controls - brief WCN / ref table TGT
Bleed air OFF
ENG ETF page
Climb if necessary
TQ 80%-85%
Retard PL non-test for 10% split and TGT in table range
TEST and Record
Bleed Air ON

Question 14

TGT Limiter / Contingency Power Check

Answer 14

120 KTAS
Anti-Ice as required
80%-85% TQ
Retard PL non-test for 10% split (110% / 60%)
2% Droop
Record TGT and TQ
Reduce COL to combined less than TQ of test engine
PL non-test IDLE (Np/Nr Split /stable Ng)
COL increase to 10 deg above limited TGT
COL reduce / PL to FLY
Anti-Ice OFF