(b)
[Ifthereisprovisionfor a secondpilot, the rotorcraft mustbe controllable with equal safety from either pilot position. Flight and powerplant controls must be designed to prevent confusion or inadvertent operation when the rotorcraft is piloted from either position;]
(c)
The vibration and noise characteristics of cockpit appurtenances may not interfere with safe operation;
(d)
In.ight leakage of rain or snow that could distract the crew or harm the structure must be prevented.
Amdt. 29-24, E.. 12/6/84
′
Elodie Roux. Septembre 2003
Subpart D : Design and Construction
FAR 29.773 : Pilot compartment view.
(a)
Nonprecipitation conditions. For nonprecipitation conditions, the following apply :
(1)
Each pilot compartment must be arranged to give the pilots a su.ciently extensive, clear, and undistorted view for safe operation.
(2)
Eachpilotcompartment mustbefree ofglare and re.ection that couldinterfere with thepilot’s view.If certi.cationfor night operationis requested, this must be shown by night .ight tests.
(b)
Precipitation conditions. For precipitation conditions, the following apply :
(1)
Each pilot must have a su.ciently extensive view for safe operation–
(i)
In heavy rain at forward speeds up to VH ; and
(ii)
In the most severe icing condition for which certi.cation is requested.
(2)
[The .rst pilot must have a window that–]
(i) Is openable underthe conditionsprescribedin subparagraph(1) ofthis paragraph; and
(ii)
Provides the view prescribed in that subparagraph. Amdt. 29-3, E.. 2/25/68
FAR 29.775 : Windshield and windows.
[Windshields andwindows must be made of material that will not break into dange-rous fragments.] Amdt. 29-31, E.. 10/22/90
FAR 29.777 : Cockpit controls.
Cockpit controls must be–
(a)
Located to provide convenient operation and to prevent confusion and inadvertent operation; and
(b)
Located and arranged with respect to thepilot’s seats so that thereisfull and unres-tricted movement of each control without interference form the cockpit structure or the pilot’s clothing when pilots from 5’2” to 6’0” in height are seated.
FAR29.779:[Motionande.ectof cockpit controls.]
[Cockpit controls must be designedso that they operate in accordance with the fol-lowing movements and actuation :
(a)
Flight controls, including the collective pitch control, must operate with a sense of motion which corresponds to the e.ect on the rotorcraft.
(b)
Twist-grip engine power controls must be designed so that, for lefthand operation, the motion of the pilot’s hand is clockwise to increase power when the hand is viewed from the edge containing the index .nger. Other engine power controls, excluding the collective control, must operate with a forward motion to increase power.
(c)
Normal landing gear controls must operate downward to extend the landing gear.] Amdt. 29-24, E.. 12/6/84
FAR 29.783 : Doors.
(a)
Each closed cabin must have at least one adequate and easily accessible external door.
(b)
Each externaldoor mustbelocated, and appropriateoperatingprocedures mustbe established, to ensure that persons using the door will not be endangered by the rotors,propellers, engineintakes, and exhausts whenthe operatingprocedures are used.
(c)
There must be means for locking crew and external passenger doors and for pre-venting their opening in .ight inadvertently or as a result of mechanical failure. It mustbepossibleto open externaldoorsfrominside and outsidethe cabinwith the rotorcraft ontheground eventhoughpersons maybe crowded againstthedoor on theinside of the rotorcraft.The meansof opening mustbe simple and obviousand so arranged and marked that it can be readily located and operated.
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本文鏈接地址：FAA規(guī)章 美國(guó)聯(lián)邦航空規(guī)章 Federal Aviation Regulations 5(43)
