II Normal Procedures Flashcards by What_If All

In the event of ICS failure, the pilot requesting control will ___, and the pilot relinquishing control will ___.

shake
raise both hands

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Use ___ procedures if qualified maintenance personnel are not available

Strange Field Procedures

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[Before Exterior Inspection]

WARNING: To preclude inadvertent seat firing, ensure ejection seat handle safety pins are ___ and ejection seat handle safety pin warning streamer is ___ of ejection seat handle before proceeding with inspection

installed
free and clear

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[Before Exterior Inspection]

CAUTION: Failure to close and latch the CFS pin storage box prior to closing the ___ may damage the ___ when the ___ is closed

canopy
canopy
canopy

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[Before Exterior Inspection]

WARNING: With starter engaged (switch in AUTO or MAN), propeller will begin to rotate after ___

electrical power is applied

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[Before Exterior Inspection]

WARNING: Both seats will eject if the ISS is in BOTH and an unpinned ejection handle is pulled, even if ___

the other seat is pinned

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[Before Exterior Inspection]

When checking the PCL, you want to verify two audible ___ from OFF to IDLE, verify the PCL has a full range of motion, make sure the PCL can’t be moved ___ of IDLE, and then use the ___ to move it to OFF (ensuring the finger lift guard ___)

clicks
aft
cutoff finger lift
returns to its spring loaded position

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[Before Exterior Inspection]

Brake reservoir - Check (Notify maintenance if filler plug ___ band is not visible or lower ___ band shows)

green
red

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[Before Exterior Inspection]

BAT switch - ON

What are the typical EICAS messages?

GEN
CANOPY
FUEL PX
OBOGS FAIL
*PMU FAIL
*OIL PX
IAC2 FAIL
L PHT INOP
R PHT INOP
*PMU STATUS
STATUS BIT
TAD OFF

*denotes message will stop flashing when MASTER WARN/MASTER CAUTION switch-lights are depressed

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[Before Exterior Inspection]

Battery voltage - Check (___ VDC minimum for a battery start)

23.5 VDC

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[Before Exterior Inspection]

CFS Donor assemblies - Inspect for ___ firing plungers (BOTH)

(can cause CFS to actuate open closing canopy)

protruding

(make sure they are not protruding)

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[Before Exterior Inspection]

Ejection seat - Inspect (BOTH):

Check the condition of the parachute risers inertia reel by pulling both straps out ___ to their full extension. Don’t attempt to test the ___ ability

simultaneously
locking

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[Before Exterior Inspection]

Will lifting the MOR handle when the seat is in the plane do anything?

Yes, lifting the MOR handle can result in the initiation of the manual release sequence which can cause injury/death to personnel and/or damage to equipment

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[Before Exterior Inspection]

29.j. Ejection seat oxygen supply - Check

NOTE: The emergency oxygen cylinder will be charged to ___ psi minimum at ___F. However, indicated pressure is affected by temperature changes. To approximate acceptable bottle pressure, add or subtract ___ psi for each degree the temperature is above or below ___F

1800 psi
70F
+-3.5 psi for each degree above/below 70F

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[Exterior Inspection]

1) number of static wicks on each wing
2) Good tire condition
3) Brake wear indication
4) minimum main strut extension

1) 4
2) No red cord visible, deep cuts, gouges, visual tire pressure (round), or anything else unusual
3) Should be protruding above housing
4) 2 inches

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[Exterior Inspection]

1) Minimum nose strut extension
2) Jack-pad position
3) Open circuit breakers on Hot Battery Bus
4) Number of static wicks on empenage

1) 2.5 inches
2) Stowed (no orange visible)
3) Consult with maintenance before flight
4) 9

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[Exterior Inspection]

Propeller blades and spinner - Check

CAUTION: Do not rotate the propeller ___ to reduce IOAT. Rotating the propeller without oil pressure can ___. Slow and limited hand rotation of the propeller for ___ is acceptable

-by hand
-damage the engine
-inspection purposes

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[Exterior Inspection]

Hyd reservoir should be in the area labeled ___ or ___

FULL AC or FULL AD

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[Exterior Inspection]

Check for condition and ___ movement of trim tab with rudder movement

anti-servo

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[Cockpit (All Flights)]

WARNING: Failure to release the emergency oxygen hose from the ___ during strap-in may result in the loss of emergency oxygen system after ___

elastic sidewall strap
ejection

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[Cockpit (All Flights)]

CAUTION: Do not connect external power if battery voltage is below ___ volts. Connecting external power could cause damage to the aircraft battery

22.0 volts

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[Cockpit (All Flights)]

What lights up on the LAMP test?

-FDR lights
-red gear handle
-red and green gear position lights/door –lights
-fire lights
-MASTER WARN/CAUTION (front cockpit only)
-COM1 and COM2 transmit
-“LAMPT TEST” on EICAS

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[Engine Start]

External power shall be used to perform a normal engine start if battery voltage is less than ___ volts. Also, consider using external power when ___

23.5 volts
motoring the engine

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If IOAT is greater than ___ C but less than ___ C, the PMU will default to ___ C for all PMU function (including IOAT display).

Study These Flashcards

96 C
121 C
121 C

If IOAT exceeds ___ C, the PMU will go offline, and will not reset until IOAT drops below ___ C

121 C 121 C

[Engine Start (AUTO)] CAUTION: Failure to ensure the ___ light remains illuminated may result in damage due to the loss of the ___ feature

ST READY automatic shutdown

[Engine Start (AUTO)] CAUTION: Abort engine start if the PCL is inadvertently moved before N1 reaches ___%

60%

[Engine Start (Auto)] CAUTION: If the ST READY advisory goes out once the start switch is placed to ___, the start should be ___ to prevent potential engine damage

Auto/Reset terminated

[Engine Start (AUTO)] CAUTION: If a start attempt is aborted (PMU or manual abort), execute ___ procedure in Section III

Motoring Run

How can you abort a start if the PCL is in any position other than off?

PCL off or starter switch to auto/reset

How can you abort a start if the PCL is in the OFF position?

Starter switch to auto/reset

CAUTION: During ground operation and after the engine is started, if the PCL is inadvertently moved to cutoff and the engine is shutting down, do not attempt to relight the engine by ___ or severe damage could occur to the engine

moving the PCL to idle

[Before Taxi] 1. GEN switch - ON (warning light should ___, ___ volts or greater and positive amps)

extinguish 27 volts

[Before Taxi] 6. AVIONICS MASTER switch - ON NOTE: After turning ON the GENERATOR switch, allow approximately ___ seconds before turning ON the AVIONICS MASTER switch to allow battery amperage to stabilize

10 seconds

AOA system test LO switch displays amber donut and ___ units

10.5 +- 0.4 units

AOA system test HI switch displays green chevron, stick shaker, and ___ units

18 +- 0.4 units

[Taxi] To prevent ground resonance within the propeller, stabilized operation of the propeller in the ___ % Np range is prohibited on the ground

62-80% Np

[Lineup Check] CAUTION: Prolonged use of pilot and AOA ___ while on the ground will damage the pitot and AOA heating elements

heat

[Takeoff] CAUTION: Avoid wake turbulence. The aircraft is particularly susceptible to wake turbulence. The vortex-produced rolling moment can exceed the ___ authority of the aircraft. Allow a minimum of ___ minutes before takeoff behind any larger type aircraft or helicopter. Attempt to remain ___ and ___ of the preceding aircraft's flight path. Wake turbulence will be most pronounced during conditions of calm, or near calm, surface winds.

aileron 2 minutes above and upwind

[Normal Takeoff] At Vr initiate rotation to ___ degree pitch attitude. If gusty winds are present, increase rotation speed by ___ the gust factor (up to ___ knots)... Distances from performance charts are predicated on setting ___% torque, releasing brakes and setting takeoff power

7-10 degrees 1/2 the gust factor (up to 10 knots) 30% torque

[After Takeoff] Charted climb performance is based on ___ KIAS If obstacle clearance or noise abatement are not factors, ___-___ KIAS will result in improved forward visibility during the climb

140 KIAS 160-180 KIAS

[Climb (Passing 10,000 Feet)] NOTE: With canopy defog ON, expect an increase in ITT of up to ___ C for a given PCL setting. At high power settings, this may exceed ITT limitations

40 C

[Climb (Passing 10,000 Feet)] NOTE: If readings other than ___ +- ___ psi are encountered at or above 18,069 feet PA, notify maintenance

3.6 +- 0.2 psi

[Descent] The descent checklist is intended to be executed prior to entering the terminal environment after aerobatics have been performed or after transiting greater than ___ NM

100 NM

[Holding] The recommended holding speed is ___-___ KIAS in clean configuration but no slower than maximum endurance speed of ___ KIAS

125-150 KIAS 125 KIAS

[Instrument Approaches] The aircraft is considered Category "___" for determination of instrument approaches

[Before Landing] NOTE: Prior to landing, set pressurization switch to DUMP if landing field elevation is above ___ MSL

7500' MSL

[Normal Landing] Airspeed will be dissipated in the flare, and touchdown will normally occur approximately ___ knots below the landing approach speed

7 knots

[Normal Landing] Upon touchdown, smoothly lower the nose gear to the runway once airspeed is below ___ knots unless needed to affect stopping distance

80 knots

[Normal Landing] CAUTION: No-flap landings with excessive sink rates greatly increase the likelihood of ___ strikes

tail strikes

[Normal Landing] CAUTION: Most blown tires occur prior to spin-up or below ___ knots. Holding excessive brake pressure as the aircraft slows below ___ knots may result in locking the brakes and blown tires

40 knots 20 knots

[Normal Landing] N1 will automatically reduce from flight idle (___%) to ground idle (___-___%), approximately ___ seconds after touchdown

67% 60-61% 4 seconds

[Maximum Braking] A smooth, ___ application, ____ as airspeed decreases, offers the best braking opportunity

single increasing

[Maximum Braking] WARNING: After a landing which required maximum effort braking and if overheated brakes are suspected, do not taxi or park in a congested area until the brakes have had sufficient time to cool. Do not set ___

parking brake

[After Landing] WARNING: In the event of a dropped ejection seat safety pin, do not use the ___ to attempt to safe the ejection seat. (they are not interchangeable, and it may not stop the ejection sequence if the handle is pulled)

CFS handle safety pin

[Engine Shutdown] NOTE: Allow ITT to stabilize at idle for at least ___ prior to shutdown

1 minute

[Engine Shutdown] NOTE: Ensure the propeller has ___ prior to securing the exterior strobes and/or navigation lights

stopped

[Before Leaving Aircraft] 4. Oxygen hose and communication cord - Stow with loop ___ CAUTION: Damage may occur to oxygen hose if stowed with loop facing ___ and in contact with the canopy strut

forward aft

II Normal Procedures Flashcards

(58 cards)