Term
| Checks _____ required between individual maneuvers if flown in a series. |
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Definition
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Term
| Tactically, a ______ check is typically performed when entering or exiting a hostile area. |
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Definition
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Term
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Definition
F - Fuel (balance and quantity).
E - Engine (within limits).
N - NAVAIDs (GPS/EHSI set); N - NACWS (check range setting and clear the airspace).
C - Communication (frequencies set, radio call according to local directives). Checks complete (climb, ops, pre-stall, spin, aerobatic, descent).
E - Equipment (G-suit test as required, loose items stowed). Emergency airfield options reviewed. |
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Term
| A _____ check is an excellent memory aid for checklist steps required prior to stalling, spinning, or aerobatic maneuvers |
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Definition
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Term
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Definition
C - Clear the area (also CWS panel clear).
L - Loose items stowed.
E - Engine (within limits).
F - Fuel balance (within 50 pounds). |
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Term
| To avoid gray out, blackout, or G-induced loss of consciousness (GLOC), an effective ______ maneuver is essential |
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Definition
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Term
| Perform a G-awareness exercise or AGSM demonstration before accomplishing any maneuver that may require _____ or more Gs. |
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Definition
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Term
| AGSM: Continue to strain and simultaneously breathe approximately every ____ seconds |
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Definition
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Term
| Do not hold the strain too long (more than ___ seconds) without breathing as this reduces G tolerance. |
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Definition
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Term
| If gray out occurs at the onset of G forces, application of the AGSM may not eliminate the gray out. If altitude or airspeed are not critical, what should you do? |
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Definition
| return to 1 G flight, reapply the anti-G strain, and then continue maneuvering |
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Term
| It is important to start the AGSM _____ the onset of G forces and maintain the strain throughout the period of increased G loading |
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Definition
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Term
| The Gx is flown at gradually increasing G levels, starting at ___ Gs and increasing to ___ Gs, depending on proficiency |
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Definition
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Term
| The AGSM cycle should last from ______ seconds with at least ______ breathing cycles |
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Definition
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Term
| Gx: use approximately ___-___knots minimum for a level to slightly descending turn where the nose remains within ___ degrees of the horizon |
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Definition
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Term
| For advanced aerobatic and formation training, the Gx exercise should be flown to G loads of ___-___ Gs |
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Definition
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Term
| If personal G tolerance is deemed insufficient for the sortie:, |
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Definition
| terminate high-G maneuvering and consider terminating the mission |
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Term
| __________ such as cities, lakes, road intersections, terrain, etc., are the primary means of maintaining area orientation |
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Definition
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Term
| When visual references are inadequate, or to augment visual orientation, the ___ or ____ with ___ may be used. |
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Definition
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Term
| two primary methods to maintain area orientation that utilize VOR or DME: |
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Definition
Center Radial (course) Method
Pie-in-the-Sky Method |
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Term
| When center radial is set, the course arrow points ____ from the NAVAID; when center course is set, the course arrow points ____ the NAVAID |
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Definition
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Term
| The center of the area (laterally) is always ____ the course deviation indicator (CDI). This method (center radial method) is best suited for areas that are ___ radials wide or less. |
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Definition
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Term
| Pie-in-the-Sky Method: Best used in ___ areas (_____ wide or more). |
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Definition
| wide ; 20 radials or more |
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Term
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Definition
| Set one boundary (course) in the CSW and mark the other boundary (course) with the heading marker. Keep the head of the bearing pointer, which always falls, between the head of the course arrow and the heading marker. |
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Term
| EFIS and GPS Display Options: Normally, a typical display setup is used until proficiency is demonstrated (the ____ page of the GPS control head in conjunction with the ___ and _____) |
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Definition
Super Nav 5 page
VOR and visual references |
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Term
| Energy level is defined by airspeed (_____) and _____(potential energy) and is manipulated with _____,_____, and ______. |
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Definition
kinetic energy
altitude
power, drag, and G loading |
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Term
| ____ feet of altitude equals approximately ___ knots of airspeed with the canopy bow on the horizon and power at maximum |
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Definition
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Term
| Altitude for Airspeed method: |
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Definition
| MAX power with the canopy bow on the horizon |
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Term
| Airspeed for Altitude method: |
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Definition
| MAX power, wings level, and clock on the horizon |
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Term
| optimum energy for aerobatic maneuvering is ___-___ KIAS at an altitude _____. |
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Definition
180 to 200 KIAS
midway between the top and bottom area limits |
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Term
| Energy may be decreased with: |
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Definition
low power settings
increased drag (e.g., speed brake) increased AOA (G loading). |
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Term
| Energy gain is enhanced with: |
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Definition
low AOA (avoid flight near zero G
high power |
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Term
| The best method to gain large amounts of energy is: |
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Definition
| a climb at 140 to 160 KIAS with MAX power |
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Term
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Definition
spins
traffic pattern stalls
cloverleaf
split-S
nose-low recovery
ELP stalls
high G turns with lower power settings |
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Term
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Definition
power-on stalls
nose-high recovery
stability demonstration
Chandelle |
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Term
| Power-On Stalls Parameters: |
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Definition
Entry: ~160 KIAS
Torque: 30-60%
Pitch: 15-40* (15-30 low,30-40 high)
Bank: 0* straight, 20-30* banking
Alt req: +1.5-2k
Recovery: Max, relax, roll |
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Term
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Definition
Entry: 125 KIAS CLN, 120 KIAS CFG
Torque: 4-6%
Pitch/bank: to maintain 120 w/ 30* bank
Alt req: -4k
Recovery: 1/2 prop arc CLN, full arc (~8*NL) CFG |
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Term
| ELP altitude losses per phase of flight w/ stall indications at recovery: |
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Definition
Glide to HK: 300ft
HK to LK: 800ft
LK to RWY: 900ft |
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Term
| If an ELP stall between low key and the RWY is encountered during an actual FL, consider ____. |
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Definition
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Term
Traffic Pattern Stall Parameters:
Overshooting & Undershooting |
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Definition
Entry: 120 KIAS CFG
Torque: 30-35% at initial, 10-15 FNL TRN, IDLE to initiate
Pitch/Bank: OVR SHT 40-45*, UND SHT 15-20*
Alt req: -2.5k |
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Term
Traffic Pattern Stall Parameters:
Landing attitude |
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Definition
Entry: 5-10 KIAS above final approach airspeed
Torque: Idle to initiate
Pitch/Bank: LDG attitude (simulate flare)
Alt req: -2.5k |
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Term
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Definition
| Simultaneously and smoothly relax back stick forces as necessary to alleviate the approach to stall indication, advance the PCL to MAX, and use coordinated rudder and aileron to level the wings. Disregard pattern ground track. Minimize altitude loss by maintaining recovery AOA until recovery is complete. While the recovery AOA is approximately 15.5 to 18 units, the primary reference for maintaining recovery AOA is a positive, vertical nose track. Recovery is complete when the aircraft is wings level and safely climbing. |
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Term
| Closed Pull-Up Stall (Simulator Training Only): On departure leg, with ___ KIAS, roll and pull, simulating an overly aggressive closed pattern. At the first approach-to-stall indication, recover by: |
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Definition
140 ;
reducing back stick pressure and rapidly rolling wings level with rudder and aileron |
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Term
| Break Stall (Simulator Training Only): At ____ KIAS, retard the PCL to approximately ___ percent torque and enter a ___-degree bank turn. Midway through the turn, increase the bank and back stick pressure until an approach-to-stall indication is recognized. Recover by: |
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Definition
200 KIAS; 10%; 60*
using stick forces as necessary to decrease the AOA. Adjust the bank angle as necessary and continue the turn to a simulated downwind leg |
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Term
| Propeller and gyroscopic effects will force the nose to the _____ when the power is increased from idle to MAX at slow speed |
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Definition
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Term
Anticipate left nose movement to
start approximately ___ seconds after moving the PCL to MAX. The slower the airspeed at recovery, the _____ the yaw will be at engine spool up |
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Definition
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Term
| Slow Flight UP parameters: |
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Definition
Airspeed: 90-95
Torque: 25%
Pitch: 10*
CONFIGURED
Bank: 20* one direction, 40* the other
Alt req: LVL (Neutral energy maneuver) |
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Term
| Slow Flight T/O parameters: |
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Definition
Airspeed: 85-90
Torque: 30%
Pitch: 9*
CONFIGURED
Bank: 20* one direction, 40* the other
Alt req: LVL (Neutral energy maneuver) |
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Term
| Slow Flight LDG parameters: |
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Definition
Airspeed: 80-85
Torque: 35%
Pitch: 8*
CONFIGURED
Bank: 20* one direction, 40* the other
Alt req: LVL (Neutral energy maneuver) |
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Term
SCATSAFE Maneuver (stands for):
***There is a long description for each letter... read it pg.103, 11-248*** |
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Definition
S - Straight and Level
C – Coordination Exercise
A - Adverse Yaw
T - Torque and Turns
S - Steep Turns
A - Abrupt Control Movement
F - Flap Retraction
E – Effectiveness of Controls |
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Term
| Stability Demo parameters: |
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Definition
Airspeed: 160 KIAS
Torque: 60%
Pitch: 40-45*
Alt req: +2k
@80 KIAS or stick shaker- IDLE, neutralize controls, let nose drop over until positive pressure is felt on stick. Maneuver complete when returned to LVL flight |
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Term
| During Stab Demo & in general: Avoid near zero-G flight for more than ___ seconds due to engine operating limitations. |
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Definition
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Term
| During Stab Demo recovery: Cross-check the G meter and maintain slightly more than ____ Gs with a small amount of back pressure on the control stick to avoid exceeding engine operating limits. |
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Definition
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Term
| Section ___ of the flight manual contains detailed information about departures from controlled flight. Additional information and details on the recovery procedure are found in section ___ of the flight manual |
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Definition
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Term
| departures from controlled flight are also referred to as _____. |
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Definition
| out of control flight (OCF) |
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Term
| Eject if it appears the aircraft is not recovering by minimum uncontrolled ejection altitude (_____ feet AGL). |
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Definition
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Term
| On most contact sorties where OCF recoveries are performed, recovery will be initiated within ____ turn of the application of rudder |
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Definition
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Term
| Due to the potential for aeration of the oil system during spin entry, do not push to less than ___ or allow the aircraft to sink before intentionally entering a spin. Allow ___ seconds of stabilized ___ flight prior to spin entry |
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Definition
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Term
| OCF (spin) entry parameters: |
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Definition
Initiate entry: 120 KIAS min
Spin entry: 80 KIAS
Torque: Idle
Pitch: 15-40*
Flight controls at spin entry:
Rudder: Full deflection in spin direction
Elevator: Full aft stick
Ailerons: Neutral
Alt req: +1k / -3.5K |
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Term
| Intentional Spin Entry (Emphasizing Near Steady State Spin Recognition and Recovery). Recoveries from these spins will utilize OCF recovery procedures and be initiated from a near steady state spin (between ___ and ___ turns from rudder application) |
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Definition
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Term
| Nose high recovery procedures: |
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Definition
| Set power to MAX and initiate a coordinated roll with back pressure to bring the nose of the aircraft down to the nearest horizon. Depending on initial airspeed and aircraft attitude, a wings-level, inverted attitude may be reached. As the nose approaches the horizon, roll to an upright attitude |
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Term
| Nose low recovery procedures: |
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Definition
| Roll the aircraft toward the nearest horizon, level the wings, then pull-up to obtain level flight using up to the maximum allowable G force. Use power and speed brake as required. |
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Term
| During a nose low recovery, do not exceed maximum allowable airspeed of ____ KIAS. |
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Definition
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Term
| Nose low recovery technique: Approaching ___ KIAS or greater, select idle and speed brake. |
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Definition
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Term
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Definition
rolling in the shortest direction to set the aircraft in an upright, wings-level attitude, adding power as required.
Roll to the nearest blue! |
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