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42 Cards in this Set

  • Front
  • Back
Abnormal ITT During Shutdown
Rapid Rise in ITT, Smoke, Flames
1.Emergency Engine Shutdown – EXECUTE
2.Ignition Switch – HOLD OFF
3.Starter – ON (monitor for normal shutdown)

If condition persists or engine fire light illuminates
4.Starter – OFF
5.Emergency Exit - EXECUTE
Abnormal Start
Watch for HOT, HUNG, or NO START
1.Condition Lever – FUEL OFF
2.Ignition Switch – HOLD OFF (starter continue engaged)
3.Starter – OFF (after 20 seconds)
4.Ignition Switch – RELEASE
(Caution) Secure starter before releasing IGN switch
Do not attempt another start until cause is corrected
Aborting Takeoff
1.PCL – FULL BETA
2.Wheel Brakes – AS REQUIRED

(Warning) Simultaneous braking, shuttle valve neutralizes
(Note) Lower nose wheel before max braking. Smooth increasing application as speed decreases. Avoid locking tires. No BETA with Engine Failure

If going into unprepared terrain:
3.Canopy – EMERGENCY OPEN
4.Emergency Engine Shutdown – EXECUTE

When aircraft comes to rest:
5.Emergency Exit – EXECUTE
Airstart
1.PCL- IDLE
2.Emergency fuel shutoff handle- DOWN
3.Standby fuel pump switch- ON
4.Starter- ON
5.N1 and ITT- MONITOR FOR START INDICATIONS
6.Starter- OFF (when ITT peaks or no indications of start)
7.Standby fuel pump-OFF (if start unsuccessful)

(Note) If attempt and unsuccess, may not be battery for flaps/gear

If start is successful:
8.Condition lever- FULL INCR
9.PCL- ADVANCE (as required)
10.PEL- EXECUTE
11.Autoignition- ON
Bailout
1.Notify Crewmember
2.Canopy – EMERGENCY OPEN
(Note) Canopy open 2 inches less, takes up to 4 sec
3.Radio Cords and Oxygen Hose or Mask – DISCONNECT
4.Harness – RELEASE

From a crouched position:
5. DIVE toward the trailing edge of either wing

When clear of the aircraft:
6. PULL parachute D-ring

Addition Items:
a)Airspeed – SLOW TO 90 TO 120 KIAS
b)Seat – LOWER PRIOR TO OPENING CANOPY
c)MAYDAY/7700 – BROADCAST
d)Emergency Engine Shutdown – EXECUTE
e)Turn toward unpopulated area.

crew,canopy,cords,mask,harness,crouch,dive,pull
Battery Failure in Flight
1.Battery switch- OFF
2.Maintain normal flight proced. Land as soon as practicable
Battery Failure on Ground
1.Battery switch- OFF
2.Return to parking spot and secure
Bleed Air Warning Light Illumination
1.Cockpit environmental control lever- FRESH AIR INCR

(Note) If light remains illum w/ cool air coming out, false indication

2.If light remains illuminated w/ hot air coming out, land as soon as practicable using normal procedures
Brake Failure
1.Aircraft – STOP, using other cockpit brakes

(Warning) Simultaneous braking, shuttle valve neutralizes
(Note) Pumping brakes may restore braking action
(Note) Brakes in other cockpit may still function

If solo or other cockpit brakes are ineffective:
2.Aircraft – Maintain directional control and stop aircraft utilizing BETA, rudder, and remaining brakes.

If going into unprepared terrain:
3.Emergency Engine Shutdown – EXECUTE

(Warning) Initially accelerate as prop feathers
(Warning) Do not attempt to taxi with brake failure, Chock b4 shtdwn if held with BETA

When aircraft comes to rest:
4.Emergency Exit – EXECUTE
Compressor Stalls
1.PCL- SLOWLY RETARD TO JUST BELOW STALL THRESHOLD TO CLEAR STALL
2.Cockpit environmental control- FULL FORWARD

(Warning) Avoid unnecessary PCL movement, advancing may cause more stalls/flamout, retarding may limit power available

3.PCL- SLOWLY ADVANCE (as required)

If the resultant power available is insufficient to execute a PEL:
4.Engine Failure- EXECUTE
If sufficient power is available:
5.PEL- EXECUTE

(Warning) Use of manual fuel control aggrevate stalls/flameout
(Warning) When engine so underpowered high rates of descent do not delay feathering or may not reach landing site
(Note) If situation permits rec: Alt, OAT, max ITT, and duration
(Note) W/ rate of descent less than feather (600-800fpm) consider allowing engine to operate until field is made
Ditching
1.Flying Speed – MAINTAIN (100 KIAS minimum)
2.Landing Gear and flaps – UP (flaps down for immediate ditch)
3.Engine Instruments – CHECK

(Warning) If Rollback, LOSS OF USEFULL POWER Procedures, If Compressor bleed valve malfunction, COMPRESSOR STALL Procedures

4.Condition Lever – FTHR
5.Landing Direction – SELECT
6.Harness – LOCKED
7.Airstart – PERFORM (if situation permits)

If airstart is not attempted or is unsuccessful, altitude permitting:
8.BAIL OUT – EXECUTE (as desired)

If ditch is to be continued:
9.Emergency Engine Shutdown – EXECUTE
10.Flaps – DOWN
11.Canopy – EMERGENCY OPEN

Additional Items:
a.MAYDAY/7700 – BROADCAST
b.Parachute – UNFASTEN
c.Oxygen Mask – REMOVE
d.Battery Switch – OFF

(Note) Consider battery on at night

As soon as all motion stops:
12.Emergency Exit – EXECUTE
13.LPU – INFLATE WHEN CLEAR OF AIRCRAFT

(Warning) Do not inflate LPU until clear of aircraft. If lanyard connected, parachute will pose a hazard to you.
(Note) If time permits, retrieve first-aid kit
Electrical/Unknown Origin Fire (IMC)
Attempt to locate/isolate the source of fire/fumes

If unsuccessful continue:
1.Utility Bus Switches- OFF

(Note) Lost: Oil press & temp, flap power & position indicator, RMI compass and cards, NACWS, transponder, VOR, TACAN, GPS, fuel quantity, BETA, utility/console/console flood/ instrument flood lights, vent blowers, scavenge pump, prop test, condenser blower, AC clutch, avionics cooling fan

2.All other nonessential equipment- OFF
3.100-percent oxygen- DON (as required)
4.Airspeed- REDUCE (as required)

(Note) Under varying conditions of altitude, fire, smoke, or fumes, pilot has option of using 100% O2, opening canopy, and/or closing O2 cylinder valve as dictated by judgment

5.Cockpit environ control/aft cockpit outside air- OFF

If fire persists:
6.Bail out (altitude permitting)

If fire extinguishes:
7.Land as soon as possible

(Note) If landing with utility bus switches secured, allow additional time to handcrank landing gear and plan for no flap landing w/ no BETA
Electrical/Unknown Origin Fire (VMC)
Attempt to locate/isolate the source of fire/fumes

If unsuccessful continue:
1.Battery and generator switches- OFF
2.100-percent oxygen- DON (as required)
3.Airspeed- REDUCE (as required)

(Note) Under varying conditions of altitude, fire, smoke, or fumes, pilot has option of using 100% O2, opening canopy, and/or closing O2 cylinder valve as dictated by judgment

4.CEC/aft cockpit outside air- OFF

If fire persists:
5.Engine Fire- EXECUTE

If fire extinguishes:
6.Land as soon as possible
7.Restoring electrical power- EXECUTE

(Note) If landing with power secured, allow additional time to handcrank landing gear and plan for no flap landing w/ no BETA
Emergency Engine Shutdown
Chip light, abnormal noise/vibration, oil system failure, prop failure, strike of ground object, departing prepared surface

1.Condition lever- FUEL OFF
2.Emergency fuel shutoff handle- PULL

(Note) After EFSH pulled do not reset on ground until cause determined and corrected
Emergency Exit
1.Canopy- OPEN (emergency open, as required)
2.Battery- OFF
3.Harness, cords, mask- RELEASE
4.Parachute- UNFASTEN
5.Aircraft- EVACUATE

(Warning) If evacuate while wearing parachute w/ lanyard connected, will deploy, possibly inflating and dragging pilot, possibly into fireball
Emergency Landing Gear Extension
1.LDG Gear PWR and CONT circuit breakers – PULL
2.Gear Handle – DOWN
3.Clutch Knob – UNLOCK
4.Clutch Knob - Engage

5.Gear – Crank down until handle stops
6.Gear Indicators – CHECK

Crank Handle until it stops
(Caution) If Crank Handle won’t turn when clutch engaged, motor is restricted. Rock Crank Handle clockwise/then counterclockwise as last resort. Report to maintenance.
(Note) If no Nose Gear with Mains D/L, land this configuration
(Note) If difficult to engage/disengage clutch, rotate crank fore and aft, reattempt
(Warning) Disengage clutch once Gear Down. If motor functions with clutch engaged, crank handle will spin, causing injury or system damage. Report to maintenance.
(Caution) LGEE system stressed for extension, should not use to retract (excluding extreme situations)
(Caution) If no DC Power, LG indicators remain unsafe. Consider airborne LG Inspections
Engine Driven or Standby Fuel Boost Pump Failure
FUEL PRESS and MASTER CAUTION illuminate:
1.PEL- EXECUTE
2.Standby fuel pump switch- ON

If lights remain illuminated:
3.Descend below 15,000 feet, avoid high power settings

(Note) Log FUEL PRESS lgt time as solitary op of primary pump
Engine Failure (HAPL/LAPL)
1.Flying Speed – MAINTAIN (100 KIAS minimum)
2.Landing Gear and flaps – UP
3.Engine Instruments – CHECK

(Warning) Execute Rollback/Compressor Stalls Procedures

4.Condition Lever – FTHR (205#)
5.Landing Site – SELECT (Paved)
6.Harness – LOCKED
7.Airstart – PERFORM (if situation permits)

If airstart is not attempted or is unsuccessful:
8.No landing site available and alt permits – BAILOUT

If forced landing is to be continued:
9.Emergency Engine Shutdown – EXECUTE
10.MAYDAY/7700 – BROADCAST
11.ELP - INTERCEPT
12.Gear and Flaps – AS REQUIRED
13.Canopy – EMERGENCY OPEN

(Note)Dirt and loose obj propelled by air-blast may restrict vis

14.Battery Switch – OFF

(Note) Consider battery on at night
Engine Fire in Flight
1.Fire- CONFIRM

If fire is confirmed:
2.Emergency Engine Shutdown- EXECUTE
3.Cockpit environmental control/aft cockpit outside air- OFF

(Note) Under varying conditions of altitude, fire, smoke, or fumes, pilot has option of using 100% O2, opening canopy, and/or closing O2 cylinder valve as dictated by judgment

If fire continues:
4.Bailout- EXECUTE

If fire extinguishes:
5.Engine Failure- EXECUTE

If no fire indications:
6.PEL- EXECUTE
Engine Fire on Ground
1.Starter – OFF (as required)
2.Emergency Engine Shutdown – EXECUTE
3.Emergency Exit – EXECUTE

(Caution) Do not attempt restart until cause is corrected
Fuel Control Stuck at Minimum Flow (Rollback)
If N1 and ITT indic that a rollback cond exists (FCU stuck at min flow):
1.Condition lever- FULL INCREASE RPM
2.EPL- ADVANCE TO DESIRED POWER SETTING

(Note) When using EPL maintain N1 above 65% to improve engine response and ensure generator stays online

If resultant power availabe is insufficient to execute PEL:
3.EPL-DISCONNECT
4.Engine Failure- EXECUTE

(Warning) When engine so underpowered high rates of descent do not delay feathering. Not recommended delaying in landing configuration below landing pattern altitude.
(Note) W/ rate of descent less than feather (600-800fpm) consider allowing engine to operate until field is made

If power available is sufficient:
5.PCL-IDLE
6.PEL-EXECUTE

(Caution) No BETA with EPL, if req, EPL to IDLE/DISSCONNECT before selecting BETA w/ PCL
Fuel Leaks or Syphoning
If possibility of engine fire, flameout, or failure due to location or severity of the leak
1.PEL- EXECUTE

If engine indications are normal
2.Land as soon as Practicable

If fuel fumes are present in the cockpit
3.Smoke or Fume Elimination- EXECUTE (as required)

(Note) Pilot has option of securing switches (landing lights, navigation lights, strobe lights, pitot heat) and CBs (LOW FUEL, LDG GEAR POSITION, LDG GEAR WARN, FUEL QTY LEFT/RIGHT. AOA INST PWR, RMI COMP) that control power to the wing
(Note) Due to stability of jet fuel, risk of igniting fuel or fuel fumes from electrically lowering gear/flaps is extremely remote.

If the pilot elects to lower the gear manually and execute a No Flap landing:
4.Landing Gear Emergency Extension- EXECUTE

(Note) landing gear indicators will remain unsafe if CB pulled, consider visual inspection
Generator Failure
1.Starter switch- OFF (both cockpits)
2.Generator switch- ON (reset)

If annunciator remains illuminated
3.Electrical Control- TAKE COMMAND
4.Generator switch- ON (reset)

If generator does not return to line:
5.Electrical Load- REDUCE

(Warning) Intsrmnt flight not possible with pwr loss, 20 min batt
6.Land as soon as practicable
Hard Landing
In the event of a hard landing where possibility of gear or struct damage:

If on the runway:
1.Full Stop- EXECUTE

If airborne:
2.Landing gear- LEAVE DOWN
3.Airborne landing gear inspection- EXECUTE

If visual damage is confirmed:
4.Execute appropriate landing gear emergency procedure

If visual damage is not confirmed
5.Execute normal landing

(Warning) Min use of brakes to avoid additional loads, no taxi
Inflight Damage/Binding Controls
If damage sustained due to collision, bird, overstress, maintaining/regaining aircraft control most important. Then check engine instruments and flight controls. May warrant visual check.

1.Maintain control of aircraft, if not controllable, BAIL OUT
2.Climb- AS REQUIRED
3.Check flight characteristics above 5000ft AGL in landing configuration, decreasing airspeed in increments of 10KIAS to an airspeed at which a safe landing can be made (no slower than 80 KIAS)

(Warning) Because of unknown flight characteristics, stall may result in unrecoverable OCF. If OCF, immediately execute OCF procedure. If recovery not imminent by 5000 AGL, BAIL OUT.

4.Fly a wide straight -in appr and land as soon as possible
Interior Light Failure
With the lights extinguished:
1.Activate and use utility/emergency light
2.Check corresponding circuit breakers- IN
3.Check corresponding switches- ON
Inverter Failure
(Note) If 115VAC CB reset F/A Att Inst will work regardless of INV selected. If 115VAC CB popped, Front Att Inst works with INV #2

1.Other inverter – SELECT

If annunciator remains illuminated:
2.Electrical control – TAKE COMMAND
3.Circuit Breakers – IN (115VAC, INV relay, INV1, INV2)

(Warning) with 115VAC CB popped:
Front CP:
a.INV1 – M Caution, INV light, Att, TN
b.INV2 – No Indication
Rear CP:
c.INV1 – M Caution, INV light, Att
INV2 - TN
(Warning) INV switch operable in CP with EC
(Warning) Inst FLT not possible with loss of AC power
Oil System Malfunction/Chip Light Illuminated
Fluctuations greater that +-5 psi, oil pressure below 65 psi at >75% N1, oil pressure above 85 psi, oil temp above 100C, or chip light illuminates:

(Note) During maneuvers, as low as 10 psi for 5 sec acceptable provided oil pressure returns to normal with no secondary indications

1.PEL- EXECUTE (utilize maximum of 850 ft-lbs torque and avoid unnecessary PCL movements)

(Warning) Torque indications may be erroneous bc of reduction gearbox failure. Watch rate of climb/descent to maintain profile

(Note) 850 ft-lbs 100kt climb = ~1200fpm clean, 700fpm gear down. If indicated climb rates significantly lower, suspect erroneous torque indications and increase power cautiously to achieve proper airspeed/VSI combo. Closely monitor for secondary indications of rising ITT, high oil temp, and/or fluctuating oil press. If secondary indications of engine failure occur while on or above ELP profile, consider securing engine

If engine failure/mechanical malfunction occurs:
2.Emergency Engine Shutdown- EXECUTE
3.Engine Failure- EXECUTE

(Note) Illum of Chip Light indicates metal part. in redux gearbox
Out-of-Control Recovery
If an out-of-control condition is encountered, accomplish the following procedures:
1.Controls- POSITIVELY NEUTRALIZE
2.PCL- IDLE
3.Altitude- CHECK

(Warning) If recov cannot be accomp by 5000AGL, BAIL OUT

4.AOA, airspeed, turn needle- CHECK

(Warning) Application of spin recovery controls when not in a steady state-spin (as verified by AOA, airspeed, and turn needle) may aggravate OCF

If in steady state spin
5.Gear/flaps- UP
6.Rudder- FULL OPPOSITE TURN NEEDLE
7.Stick- FORWARD OF NEUTRAL (erect spin)
NEUTRAL (inverted spin)

(Warning) Application of power when not in steady state spin will result in rapid increase of rate of descent and airspeed
(Warning) If recovery not evident in 2 turns after inputs applied, verify cockpit indications and visually confirm proper recovery controls. Adding max power while maintaining recovery controls will enhance recovery
(Warning) If recovery not evident soon after applying inputs, pushing stick further forward may facilitary recovery

8.Controls- NEUTRALIZE WHEN ROTATION STOPS

When aircraft regains controlled flight:
9.Recover from unusual attitude

(Warning) Lower power settings reduce torque effect, restrict rapid airspeed buildup, and enhance controllablity. Howerver departures from controlled flight in close proximity to the ground may require rapid power addition upon OCF recovery
Precautionary Emergency Landing (PEL)
(Warning) Should engine failure occur at low alt, any delay in transitioning to engine failure procedures may result in high rates of descent and/or inability to reach a suitable landing site
(Note) Nearest suitable runway may include runway remaining

1.Select nearest suitable runway
2.Climb at 100KIAS or accelerate to a position within dead engine glide distance of the runway
3.Landing gear and flaps- UP (as appropriate)
4.Aircraft and engine instruments- CHECK
5.ELP- INTERCEPT

turn, climb, clean, check, determine, deliver, reduce, lower, report, high key, low key, continue, lower, decelerate
Prop RPM Fluctuations
1.PROP TEST circuit breaker- PULL

If fluctuations cease, continue flight. If fluctuations continue:
2.PEL- EXECUTE
Smoke or Fume Elimination
(Warning) Prior to any procedure that will create draft, determ source of smoke, sudden draft may cause smolder to flame

1.100-percent oxygen- DON
2.Airspeed- REDUCE (as required)
3.Cockpit environmental control/aft cockpit outside air- FRESH AIR INCREASE/ON

If smoke or fumes remain, obstructing sight for landing, or heat buildup requires ventilation:
4.Canopy- EMERGENCY OPEN

(Note) Due to stability of jet fuel, risk of igniting fuel or fuel fumes from electrically lowering gear/flaps is extremely remote. If desired, execute landing gear emergency procedure.
Prop RPM Out of Limits
1. Condition lever- ATTEMPT TO ADJUST PROP RPM TO NORMAL OPERATING RANGE

If conditions persist:
2. PEL- EXECUTE

If normal indications are restored:
3. Land as soon as practicable using normal procedures

(Warning) Advancing EPL beyond point at which fluctuations are minimized will aggravate overspeed condition which could result in catastrophic failure of power turbine.

(NOTE) If activation of primary fuel-topping governor has occurred, Py air will bleed and cause surges. EPL can lessen severity of low end fluctuations.
Split Flap Condition
1.Reset flap lever to prior position
2.Pull FLAP PWR circuit breaker
3.Land as soon as practicable

(Note) Aircraft is fully controllable in split-flap configuration. Control pressure light with full trim. Consider increased landing speed for controllability.
Strike of Ground Object
1.Emergency Engine Shutdown – EXECUTE
Tire Failure on Takeoff Roll
When still on runway:
1.Aborted Takeoff – EXECUTE
If Airborne:
2.Landing Gear – Remaining Down

(nonmemory)
3.Get visual confirmation
4.Land aircraft on good tire side of runway
5.Maintain directional control with rudder as necessary and brakes as required. Use BETA and brakes to aid in deceleration.
6.Do not taxi with blown tire.

If a tire blowout occurs during normal landing roll, use rudder and brakes for directional control and BETA and brakes for deceleration. When stopped Engine Shutdown Checklist and have aircraft towed.

(Note) If gear or wheel comes off, consider landing gear down with no nose gear or one main gear.
Torque Sensing System Failure
If erroneous torque indications are suspected or torquemeter reads zero, fly known combinations of other available engine indications, rate of climb or descent, attitude, and airspeed, and land as soon as practical using normal procedures.
Uncommanded Propeller Feathers
1.Condition lever – FULL INCREASE RPM

If propeller remains feathered:
2.PCL – ADVANCE (as required)

(Note) In the event of a primary governor shaft failure, prop will move to feather, unboosted engine oil pressure may be enough at high power settings.

If resultant power does not improve performance:
3.PCL – IDLE
4.Engine Failure- EXECUTE

(Note) Because prop may unfeather, consider leaving condition lever at FULL INCR RPM until ELP intercept

If propeller unfeathers:
5.PEL – EXECUTE
Uncontrollable High Power
Bearings of shaft in FCU could fail without prior fluct. If torque, N1, and fuel flow go to max and the engine is unresponsive to PCL mvmnt:

1.PEL- EXECUTE

(Warning) Certain failures can cause surges from max to min fuel flow. EPL will have no effect on max but may raise low end of surges

2.Friction lock knob- FULL DECREASE
3.Condition lever- Rapidly retard to FUEL OFF

(Warning) When retarding condition lever, do not hesitate in FEATHER bc high power may cause severe vibration and torque

(Note) Altitude permitting, pilot may elect to shut down ending with EFSH, engine may continue running for as long as 30 sec

4.Engine Failure- EXECUTE
Unsafe Landing Gear Indication (Gear Extension)
If a landing gear problem is encountered or suspected, the gear should never be cycled because reextending the gear could aggravate the problem.

(NOTE) Should the nosegear fail to extend fully with both main gear down and locked, landing should be attempted with both main gear down and locked using appropriate procedures.

If one or more main gear fail to extend, a gear up landing is preferred to landing with one main gear retracted. Execute the appropriate procedure. If gear position does not match the position of the landing gear handle or the red (in transit) light is illuminated, proceed as follows:
1.Landing Gear Emergency Extension – EXECUTE

If unsafe condition persists:
2.Airborne Landing Gear Inspection – EXECUTE

If visual check confirms gear unsafe:
3.Unsafe Gear Emergency Landing – EXECUTE

If visual check confirms gear down and locked:
4.Land with caution. Roll out straight ahead using brakes and BETA only as necessary. Stop on runway until gear is inspected.
Unsafe Landing Gear Indication (Gear Retraction)
If three up indications are not encountered upon gear retraction:
1.Gear Handle – DOWN

If unsafe gear indications still exist:
2.Unsafe Landing Gear Indication (Gear Extension) Procedure – EXECUTE

If gear down and locked indications:
3.Landing Gear – LEAVE DOWN
4.Land as soon as practical
Windshear/Waketurbulence Escape Procedures
Indications: +-10kts Airspeed, +-500fpm VSI, +-5deg pitch, Unusual pwr

(Note) Report windshear to ATC

If windshear is encountered:
1.Wave off- EXECUTE (Maintain current configuration and wings level until clear of windshear)

(Warning) Not recomm. to lower nose to recover airspeed