Manuevers Flashcards
Initial Hover Checks
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)
Hover Maneuvering Checks
5’-10’
90 deg right + left (CRIS)
Forward, lateral, and rearward flight (10’-15’)
FMC ATT HOLD Checks
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
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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
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Cyclic 1/2” in any direction
Note TRC symbology / return to trimmed position
Disengage holds via 6’o clock
Visonic check
ALT hold
CPG video (pick target 500m away)
TADS DAY/FLIR N FOV
90 deg turns about the nose
Hover Drift Box Check
EGIs keyed / 4 Satellites
ATT + ALT hold
Drop box (5m drift)
Initial Take Off Checks
ENG / ENG SYS page Control positions and response 30-40 Stab programming Vibrations / Instruments TQ within 5%
Cruise Checks
Straight/Level 120 KTAS
Vibrations + Fuel consumption
Note TQ
Autorotation
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
Attitude Hold Check
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)
Maneuvering Flight
120 KTAS - Note vibrations
20% torque / 120 KTAS vibrations, control placement, stability
MAX CON TQ / 120 KTAS vibrations, control placement, stability
Stabilator Check
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)
Vh Check
Increase COL to MAX CON TQ or limit / maintain ALT
Vibrations / Control / Max travel
Note TGT
ETF Check
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
TGT Limiter / Contingency Power Check
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