Section 2 - Limitations 4,5,6,7,8,9,10 Flashcards

Power Plant Limitations & Altitude and OAT Limitations

1
Q
  1. Powerplant limitations
A
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2
Q

Engine manufacturer:

A

Bombardier Rotax GmbH

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3
Q

Engine model:

A

912 S3

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4
Q

Max. T.O.

A

Max Power kW (hp)
73.5 (98.6)

Max rpm. Prop, rpm (engine)
2388 (5800)

Time max. (minutes)
5

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5
Q

Max. Cont.

A

Max Power kW (hp)
69 (92.5)

Max rpm. Prop, rpm (engine
2265 (5500)

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6
Q

Temperatures:

A

Max CHT* 135° C
Max CT 120° C
Min/MaxOil 50°C/130°C
Oil normal operating range (approx.) 90° C /110°

applicable for Engines up to serial no. 4924543(inchtded) and repaired engine which doesn’t change the cylinder head n°3 with new one (part no. 413195)

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7
Q

Oil Pressure:

A

Minimum 0.8Bar/12psi (below 1400 rpm prop)

Normal 2-5 Bar / 29-73psi (above 1400 rpm prop)

Maximum 7 Bar / 102 psi (above 1400 rpm prop)

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8
Q

Engine starting: allowable temperature range

A

OAT Min -25° C

OAT Max +50° C

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9
Q

In event of cold starting operation…

A

it is permitted a maximum oil pressure of 7 bar for a short period.

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10
Q

Fuel pressure:

A

Minimum 2.2 psi (0.15 Bar)

Maximum 5.8 psi (0.40 Bar) or 7.26 psi* (0.5 Bar)

*only applicable for fuel pump part no. 893 / /0,893 /14 or 893115.

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11
Q
  1. Lubricant
A

Use only oil with API classification “SG” or higher.
For additional info, refer to “Rotax Operators Manual’’ - last issue “Operating Media” Section.

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12
Q
  1. Coolant liquid
A

Refer to “Rotax Operators Manual” - last issue “Operating Media” Section.

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13
Q
  1. Propeller
A
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14
Q

MANUFACTURER:

A

MT Propeller

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15
Q

MODEL:

A

MTV-21-A-C-F-/CF178-05

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16
Q

TYPE:

A

wood/compositc 2-bladc, variable pitch hydraulically controlled and fully featherable

17
Q

DIAMETER:

A

1780 mm (no reduction is permitted)

18
Q
  1. Governor
A
19
Q

MANUFACTURER:

A

MT Propeller

20
Q

MODEL:

A

P-875-12

21
Q

OPERATION:

A

Hydraulically controlled (oil pressure to reduce the
pitch)

22
Q
  1. Maximum operating altitude
A

Maximum operating altitude is 14000 ft (4260 m) MSL

Flight crew is required to use supplemental oxygen according to applicable Air Operation Rules.

23
Q
  1. Ambient temperature
A

Ambient temperature: from -25°C to +50°C.

Flight in expected and/or biown icing conditions is forbidden.