NEL QUİZ

Vital Actions?

1. Flap Up / İndicator Up

2. Both Mags - On

3. Trim, Pos, Bcn - On

4. Wx light - PTT On and Off

5. Batt / Alt - On

6. Fuel Pump - On / Light - On

7. All CBs - In

8. ADF, DME, Intercom - Set

9. Ammeter - Charging / Engine Instrument - In green

10. Fuel on Both

11. Mixture - Lean

12. Pitch - Fine

13. Trimmers set for T/O

14. Fire Extinguisher and First Aid Kit - Secure

15. Latch - Vertical

RPM drop in excess of 200 RPM may indicate a ………………. or a ………………………….. .

1. Faulty Magneto

2. Faulty Ignition System

For a constant “G” pullout from spin, height lost is around ………….. .

700

Throttle lever must not be moved unless mixture lever is in full rich position and electric fuel pump is “ON”, else it would result in ……………………………. .

Scoring Idle Valve

In case of complete electrical failure fully charge battery can sustain for …………. with full loads and ………….. with reduced loads.

1. 7 to 8 min

2. 20 min

Steps in case of Canopy Warning Lt ON in first cross wind?

1. Discontinue maneuver

2. Maintain st and lvl attitude

3. Reduce speed to 100 kts

4. Give call to Caravan

5. Head towards long finals

6. Pull out stall Wx Cb

7. Do not touch canopy handle

8. Not fly over populated areas

9. Avoid +G/-G

10. LASAP via St-in approach

11. Clear the R/W

12. Switch off at ‘D’ facing west

Steps in case of Partial power after Takeoff?

1. Maintain 80 kts climb altitude till 1500’

2. Turn towards lowkey

3. Give call to caravan

4. Kepp climbing and perform trouble cx

5. In case of no joy keep heading to lowkey

6. Prior lowkey take SFO settings

7. Give call for lowkey and land through SFO

8. Clean the R/W

9. Switch off at ‘D’ facing west

A flick in fuel flow needle a maximum and then dropping zero is an indication of …………………. .

Fuel starvation

What are the three primary factors of engine failure?

1. Fuel starvation

2. Ignition Problem

3. Mechanical Failure

Wind Limits

Solo: Hw-13kts, Xw-5 kts, Tw-5kts

Training: Hw-25, Xw-13, Tw-7

Probeller blade angles for low pitch is 13.5deg abd for high pitch is 27.5deg when measured at 30 inches’ radius.

T / F

True

Maximum weight permitted to each seat baggage compartment is ………. .

100 kg

Oil Temp Limits?

Min: 120F

Normal: 165-220F

Max: 245F

Step in case of High CHT Cylinder 5?

1. Mixture rich

2. Lower attitude

3. Discontinue if in climb

4. If still high

5. Reduce power 18/21

6. LASAP via SFO over run airfield

Base Leg CX

1. Throttle Idle(touch of left rudder)

2. Mixture rich

3. Pitch fine

4. Fuel pump on

5. Landing Light on

6. Speed below 105 kts flaps 20deg

7. Hold height

8. 90 kts lower nose to maintain 85kts

9. Throttle 1600/1700 RPM

10. Trim the A/C

11. Re-check power, maintain speed with attitude

12. T/D 2 o’clock, initiate base turn

RPM Limits

Idle: 900-1000

Taxi: 1000-1200

Windmill: 1100-1200

T/O: 2600-2700

Max: 2700

Overspeed: 2700-2900

RPM rise Mix cx: 10-30

Write down egress procedure

1. Throttle idle

2. Mixture idle cut off

3. Fuel off

4. Batt/Alt off

5. Both Mags off

6. Parking brake in

7. Headset and harnesses remove

8. Canopy unlock and open

9. Evacuate

Turns with 45deg to 60deg angle of bank, during a glide, significantly increase the margin above stalling speed.

T / F

False

Fan stop actions?

1. Throttle full open (no joy)

2. Glide 80 kts

3. Select a field +- 30deg from nose

4. Mixture rich

5. Pitch fine

6. Fuel on both

7. Fuel pump on

8. Re-cx throttle full open (no joy)

9. Harnesses tight and locked

10. Flaps as required

11. Land straight ahead turning +- 30deg and max 30 AoB

In LASAP you have to land at your nearest airfield

T / F

True

Pre Takeoff Cx?

1. Front A/C getting airborne or no A/C in front

2. Give call “Call sign, Takeoff”

3. Ref point selected

4. Control column neutral

5. Ready to roll

Steps for Partial power in first crosswind?

1. Maintain 80 kts climb attitude

2. Head towards lowkey point

3. Perform trouble cx

4. Give call to Caravan

5. Keep climbing to lowkey

6. Prior lowkey take SFO setttings

7. Abeam lowkey give call

8. Cx ht at lowkey

9. Turn for basekey

10. Perpendicular to R/W give call

11. Shift aimpoint and cx speed

12. If high reduce power, still high throttle idle, still high shift aimpoint

13. Land the A/C, clear the R/W

Steps in case of Bird Hit in downwind?

1. Visually inspect wings and flaps

2. Confirm A/C stable

3. Give call “Caravan, 406, birdhit, A/C stable”

4. Perform controllability cx

5. Determine min controllability speed. Do not go below 70 kts

6. If during approach A/C is unstable, go around make another approach with higher speeds

Steps in case of Flameout after T/O below 500 ft AGL?

1. Throttle full open

2. Glide 80 kts

3. Select a field +-30deg from nose

4. Mixture rich

5. Pitch fine

6. Fuel on both

7. Fuel pump on

8. Re-cx throttle full open. No joy

9. Harnesses tight and locked

10. Flaps as required

11. Land straight ahead by turning +-30 deg and max 30 AoB

12. Short of T/D feet of rudder pedals

13. Carry out egress

Oil pressure limits

Start and warmup : 25 - 115 PSI

Min : 25 PSI

Min in cruise : 55 PSI

Normal : 55 - 95 PSI

Max : 95 PSI

Periodic cxs are conducted after every ……………….. mins of flight

15

With steady drop in oil pressure it will take ……………. for engine to fail.

less than 10 min

CHT limits

Min : 150 F

Normal : 225 - 470 F

Max : 500 F

Max at start : 400 F

Self-cleaning temperature of spark plugs is ……………….

450deg C

Procedure to clear rough run during Run Up cxs

1. Throttle 2000 rpm

2. Mixture lean

3. Punch clock for 20sec

Steps in case of High Oil Temperature?

1. Eng Ts and Ps monitor closely

2. RPM confirm governed at selected

3. If oil temp >220F, set min practical power 18/21. Min st and lvl spd 90 kts

4. Lower attitude to increase airspeed

5. If oil pressure <55 psi, perform low oil pressure drill

6. LASAP via SFO

Anti-Embarrassment cx

1. Flaps up / indicator up

2. Landing lt - off

3. Frequency set to ATC freq

Actions in case of inadvertent opening of engine cowling or baggage compartment door?

1. Reduce spd tp 100 kts

2. Give call to caravan

3. Visiually inspect for any damage

4. Head toward airfield

5. Land back through st-in approach

6. After landing clear the R/W

Fuel flow limits

Idle : 1.5 - 3 GPH

2000 RPM : 10 - 12 GPH

Normal : 9 - 22 GPH

T/O : 21 - 25 GPH

Max : 27 GPH

Normally, with short take-off distance of the A/C, abort is not a problem unless ………………… is a factor

Direction control

…………….. should be used on wheel fire; this prevents the rapid cooling and contraction of the metal

DCP

Non adherence to correct lift off speeds during takeoff could result in possibility of …………………..

touching down again and imposing side stress on the landing gears

Write down the steps of abort procedure?

1. Throttle idle

2. Lower nose ( if applicable)

3. Apply brakes

4. Maintain direction

5. Give call “ 321 aborting, 321 aborting”

6. A/C stops

7. Switches off, delta or taxiback as applicable

Oil pressure should be indicated within …………….

30 seconds

Write down the downwind cx

1. Area from left clear

2. Flaps up / indicator up

3. Wx light - PTT all lights on and off

4. Area from front clear

5. Mixture as reqiured

6. Fuel pump on

7. Fuel on both

8. Left tank …., right tank…., imbalance….

9. Area from right clear

10. All CBs in

11. Ammeter charging, engine instrument in green

12. Area from right, top to left clear

13. Left fuel cap secure / no drainage sir pls cx yours

In case of Tire Failure, land through straight-in approach

T / F

False

Difference between two Mag drops should not be more than 50 RPM

T / F

True

RPM limitation for parking brakes is 1500 RPM

T / F

True

Best rate of climb speed is …….. & best AOC speed is ……….

85 kts

65 kts

Over speed RPM is from ……… to ………

2700- 2900

Actions in case a “cut-throat” signal is given by the ground crew

1. Fuel off

2. Continue cranking

3. Hold brakes

4. Throttle full fwd

5. Mixture idle cut off

6. Do not restart the engine

Write down steps for Canopy warning light?

1. Discontinue maneuver

2. Reduce speed to 100 kts

3. Stall warning cb out

4. Do not touch canopy handle

5. Not fly over populated areas

6. Avoid ±Gs

7. LASAP to own airfield through st-in approach

Write down the indications of an Engine Failure non mechanical in air

1. Change in engine noise

2. Boost ambient

3. Loss of thrust

4. Windmill RPM

5. Fuel flow zero

6. CHT reducing

7. Engine parameters unwinding

Run up cx

-

Permissible RPM difference while checking mags ………… RPM

25 - 175

Lower threshold of spark plug nose tip temperature for effective MAG checks in run up checks is ………. degC

450

Steps in case of RPM Over speed

1. Engine Ts & Ps monitor closely

2. Throttle reduce

3. Pull out if in dive, if still high

4. RPM lever as required

5. If RPM comes within limits

6. Consider a return base

7. if RPM not within limits

8. Airspeed reduce by raising attitude

9. Throttle minimize movement, do not maneuver

10. LASAP via SFO over airfield

Steps in case of Rough Running

1. Select St & Lvl attitude and head to airfield

2. Perform analyze checks

3. Throttle as required

4. Mixture as required

5. If rough running persist

6. Throttle set for smooth running

7. Check RPM, MAP, Fuel Flow fluctuations

8. Mixture rich

9. LASAP via SFO over airfield

Things to check while approaching A/C

1. Parking suitable for start

2. Chocks in position

3. Fire extinguisher placed

4. Canopy and wing cover remove

5. Earthing cable connected

6. Crew chief present

7. Pitot cover remove and secure

Write down following

a) Design Cruising Speed ………..

b) Design Flap Speed ……….

c) Design Maneuvering Speed ……….

d) Lift off Speed …………

e) Min Unstick Speed ………..

a) 154 kts

b) 105 kts

c) 143 kts

d) 70 kts

e) 58 kts

Nose Wheel oleo extension needs to be ………… during Pre Flight

4-6 inches

Smooth drop off past the normal range during MAG checks is a sign of ……………………….

too lean or too rich mixture

If minimum oil pressure is not indicated within 20 sec, shutdown the engine.

T / F

False

Gs limits for Aerobatics in SMK?

Positive: 5.4G

Negative: -2.7G

Do not maintain climb speed below ……… after takeoff

70 kts

There is no restriction on full power climbs till the time …………………………

CHT in green

By leaning the mixture to best power the airspeed will increase by ………………

4-5 kts

In the event of an engine failure, the oil pressure may indicate ……………..

50 - 55 psi

With propeller stop in air, the ……… will reduce as propeller is not wind milling.

Drag

If fuel flow fluctuations are accompanied with RPM fluctuations, ……………………. should be anticipated.

Engine failure

Propeller blade angles for low pitch is ……….. and for high pitch is …………. whem measured at 30 inches radius.

13.5

27.5

Nose wheel steering is +45deg

T / F

False

Vh - Max speed in level flight with max continous power …………..

Vne - Never exceed speed ………….

Vmu - Minimum un-stick speed …………….

Vr - Rotation speed …………

Vlof - Lift off speed ………….

145 kts

196 kts

58 kts

60 kts

70 kts

No flights shall be planned for a landing weight in excess of ……………..

1140 KG