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
Amount of unusable fuel supply?
2.5 Gallons/tank
26
When is it allowed to open rear door during flight? Max. airspeed with door open?
During unaccelerated and coodinated flight, max. 70 KIAS. Max. 100 KIAS with door open.
27
Procedures during airdrop?
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
Max cross wind for take off or landing on a dry runway?
30 knots