РЪКОВОДСТВО ЗА ЛЕТАТЕЛНА ЕКСПЛОАТАЦИЯ НА РОТОРКРАФТА

(a) Airspeed and rotor limitations.

Information necessary for the marking of airspeed

and rotor limitations on or near their respective

indicators must be furnished. The significance of

each limitation and of the colour coding must be

explained.

(b) Powerplant limitations. The following

information must be furnished:

(1) Limitations required by JAR

29.1521.

(2) Explanation of the limitations, when

appropriate.

(3) Information necessary for marking

the instruments required by JAR 29.1549 to

29.1553.

weight and centre of gravity limits required by

JAR 29.25 and JAR 29.27, respectively, must be

furnished. If the variety of possible loading

conditions warrants, instructions must be included

to allow ready observance of the limitations.

(d) Flight crew. When a flight crew of more

than one is required, the number and functions of

the minimum flight crew determined under JAR

29.1523 must be furnished.

(e) Kinds of operation. Each kind of

operation for which the rotorcraft and its

equipment installations are approved must be

listed.

must be furnished to allow compliance with JAR

29.1517.

(g) Maximum allowable wind. For Category

A rotorcraft, the maximum allowable wind for

safe operation near the ground must be furnished.

(h) Altitude. The altitude established under

JAR 29.1527 and an explanation of the limiting

factors must be furnished.

(i) Ambient temperature. Maximum and

minimum ambient temperature limitations must be

furnished.

(a) The parts of the manual containing

operating procedures must have information

concerning any normal and emergency

procedures, and other information necessary for

safe operation, including the applicable

procedures, such as those involving minimum

speeds, to be followed if an engine fails.

(b) For multi-engine rotorcraft, information

identifying each operating condition in which the

fuel system independence prescribed in JAR

29.953 is necessary for safety must be furnished,

together with instructions for placing the fuel

system in a configuration used to show

(c) For helicopters for which a VNE (poweroff)

is established under JAR 29.1505 (c),

information must be furnished to explain the VNE

(power-off) and the procedures for reducing

airspeed to not more than the VNE (power-off)

following failure of all engines.

(d) For each rotorcraft showing compliance

with JAR 29.1353 (c) (6) (ii) or (c) (6) (iii), the

operating procedures for disconnecting the battery

from its charging source must be furnished.

(e) If the unusable fuel supply in any tank

exceeds 5% of the tank capacity, or 3.8 litres

(0.8 Imperial gallon/1 US gallon), whichever is

greater, information must be furnished which

indicates that when the fuel quantity indicator

reads ‘zero’ in level flight, any fuel remaining in

the fuel tank cannot be used safely in flight.

(f) Information on the total quantity of

usable fuel for each fuel tank must be furnished.

(g) For Category B rotorcraft, the airspeeds

and corresponding rotor speeds for minimum rate

of descent and best glide angle as prescribed in

JAR 29.71 must be provided.