(b)
For powerplant fuel controls–
(1)
Each fuel tank selector valve control must be marked to indicate the position corresponding to each tank and to each existing cross feed position;
(2)
If safe operation requires the use of any tanks in a speci.c sequence, that sequence mustbe marked on,oradjacentto,the selectorforthosetanks; and
(3)
Each valve control for any engine of a multiengine rotorcraft must be marked to indicate the position corresponding to each engine controlled.
(c)
Usable fuel capacity must be marked as follows :
(1)
For fuel systems having no selector controls, the usable fuel capacity of the system must be indicated at the fuel quantity indicator.
(2)
For fuel systems having selector controls, the usable fuel capacity available at each selector controlposition mustbeindicated nearthe selector control.
(d)
For accessory, auxiliary, and emergency controls–
(1) Each essential visual position indicator, such as those showing rotor pitch or landinggearposition, mustbe markedsothat each crewmember candetermine at any time the position of the unit to which it relates; and
′
Elodie Roux. Septembre 2003
Subpart G : Operating Limitations and Information
(2) Each emergency control must be red and must be marked as to method of operation.
(e) [For rotorcraft incorporating retractable landing gear, the maximum landing gear operating speed must be displayed in clear view of the pilot.]
Amdt. 29-24, E.. 12/6/84
FAR 29.1557 : Miscellaneous markings and placards.
(a)
Baggage and cargo compartments, and ballast location.Eachbaggage and cargo com-partment,and eachballastlocationmusthaveaplacard stating anylimitationson contents, including weight, that are necessary under the loading requirements.
(b)
Seats. If the maximum allowable weight to be carried in a seat is less than 170 pounds, a placard stating the lesser weight must be permanently attached to the seat structure.
(c)
Fuel and oil .ller openings. The following apply :
(1)
Fuel .ller openings must be marked at or near the .ller cover with–
(i)
The word ”fuel”;
(ii)
For reciprocating engine powered rotorcraft, the minimum fuel grade;
(iii) [Forturbine-engine-poweredrotorcraft,thepermissiblefueldesignations, except that if impractical, this information may be included in the rotor-craft.ight manual,and thefuel .llermaybemarked with anappropriate reference to the .ight manual; and]
(iv) For pressure fueling systems, the maximum permissible fueling supply pressure and the maximum permissible defueling pressure.
(2)
Oil .ller openings must be marked at or near the .ller cover with the word ”oil.”
(d)
Emergency exit placards. Each placard and operating control for each emergency exit mustdi.erin colorfromthe surroundingfuselagesurfaceasprescribedinSec. 29.811(h)(2).Aplacard must be near each emergency exit control and must clearly indicate the location of that exit and its method of operation.
Amdt. 29-26, E.. 10/3/88
FAR 29.1559 : Limitations placard.
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本文鏈接地址：FAA規(guī)章 美國聯(lián)邦航空規(guī)章 Federal Aviation Regulations 5(107)
