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FLSK EK20 > DASH ONE: SECTION 5 (Limits) > Flashcards

DASH ONE: SECTION 5 (Limits) Flashcards

You should be able to tell all the limits and notes/cautions/warnings

1
Q

RPM limits

A

Normal operating range: 2200-2700RPM

Maximum 2700 RPM

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2
Q

Since instances of inadverdent overspeed do occur, reporting to then technician in charge is mandatory, if RPM exceed “…”

A

2700 for more than 2 seconds, or RPM exceed 2730 regardless of duration

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3
Q

The engine must not be operated above 2700 RPM. Doing so will result in “…”

A

“Abnormal wear on bearings, counterweight rollers and other engine parts, concluding in possible engine failure.”

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4
Q

Oil pressure

A

Normal operating range: 60-85 PSI
Caution range: 25-60 PSI and 85-100 PSI
Minimum for engine idling: 25 PSI
Maximum for engine start and warm-up: 100 PSI

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5
Q

Oil temperature

A

Normal operating range: 50-120°C

Maximum: 120°C

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6
Q

Cylinder head temp.

A

Normal operating range: 105-225°C
Caution range: 225-245°C
Maximum: 245°C

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7
Q

WEIGHT

Normal category -definition

A

AUW (All Up Weight) less than 1200kg

CG is not behind 30% of MAC

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8
Q

WEIGHT

Utility I category -definition

A

AUW (All Up Weight) less than 1125kg

CG is not behind 27,5% of MAC

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9
Q

WEIGHT

Utility II category -definition

A

AUW (All Up Weight) less than 1000kg

CG is not behind 27,5% of MAC

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10
Q

WEIGHT

Aerobatic category -definition

A

AUW (All Up Weight) less than 900kg

CG is not behind 27,5% of MAC

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11
Q

Normal category
Maneuvers?
G limits?

A
  1. Any maneuvers used in normal flight
  2. Stalls (except whip stall, hammer stall)
  3. Lazy eights, chandelles, and steep turns with angle of bank not exceeding 60°.

G limits: 4,4 positive and 2,2 negative

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12
Q

Utility I category
Maneuvers?
G limits?

A
  1. Any maneuvers used in normal category
  2. Erect stall
  3. Spins
  4. Lazy eights, chandelles, and steep turns with angle of bank exceeding 60°.

G limits: 4,8 positive and 2,4 negative

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13
Q

Utility II category
Maneuvers?
G limits?

A
  1. Any maneuvers used in utility category I
  2. Rolling
  3. Looping
  4. Half roll (Split-S)
  5. Top roll (Immelmann)

G limits: 5,4 positive and 2,7 negative

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14
Q

Aerobatic category
Maneuvers?
G limits?

A
  1. Any maneuvers used in utility category I and II

G limits: 6,0 positive and 3,0 negative

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15
Q

Maximum landing weight?

A

1140 kg

“no flight should be planned for a landing weight in excess of this limit.”

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16
Q
  • Maximum number of persons on board?

- Maximum permissible load in the rear compartment?

A
  • Max 3 persons on board OR the number of seats equipped with safety harnesses.
  • One person + 50 kg luggage / a total of 100 kg luggage / 150 kg luggage if placed on special cargo floorboard
17
Q

Inverted flight time limit?

A

10 seconds - due to engine oil system design

18
Q

During and/or immediately after inverted flight, you may momentarily experience a “…” due to air locks in the fuel system.

A

“Power loss”

19
Q

How many persons are allowed during aerobatic flight?

What is allowed in the rear compartment?

A
  • 2 persons

- Rear seat and baggage compartment must be empty.

20
Q

AIRSPEED LIMITS

SPEED - Vne

A

Vne
(Never exceed)
196 knots
Do not exceed this speed in any operation.

21
Q

AIRSPEED LIMITS

SPEED - Vno

A

Vno
(Max. structural cruising)
154 knots
Do not exceed this speed except in smooth air and then only with caution.

22
Q

AIRSPEED LIMITS

SPEED - Va

A

Va
(Max. maneuvering)
143 knots
Do not make full abrupt control movements above this speed.

23
Q

AIRSPEED LIMITS

SPEED - Vf

A

Vf
Flaps extended (1-10°)
130 knots

24
Q

AIRSPEED LIMITS

SPEED - Vfe

A

Vfe
Flaps extended (11-38°)
100 knots

25
Q

Amount of unusable fuel supply?

A

2.5 Gallons/tank

26
Q

When is it allowed to open rear door during flight?

Max. airspeed with door open?

A

During unaccelerated and coodinated flight, max. 70 KIAS.

Max. 100 KIAS with door open.

27
Q

Procedures during airdrop?

A

a) The crew members must be strapped in.
b) The drop must be performed in a downward motion, and during level flight only.

Drop of cargo from Direct Vision window may cause damage to the stabilizer.

28
Q

Max cross wind for take off or landing on a dry runway?

A

30 knots

FLSK EK20 (20 decks)

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