(b)
Each location, such as a locker or compartment, that carries any .re extinguishing, signaling, or other lifesaving equipment must be marked accordingly.
(c)
Stowageprovisionsfor requiredemergency equipment mustbe conspicuously marked toidentify the contents andfacilitate[the easy] removal ofthe equipment.
(d)
Each liferaft must have obviously marked operating instructions.
(e)
Approved survival equipment must be marked for identi.cation and method of ope-ration.
Amdt. 25-46, E.. 12/1/78
FAR 25.1563 : Airspeed placard.
Aplacardshowingthemaximumairspeedsfor .ap extensionforthetakeo.,approach, andlandingpositions mustbeinstalledin clear view of eachpilot.
50.3 Airplane Flight Manual
FAR 25.1581 : General.
(a)
Furnishing information. An Airplane Flight Manual must be furnished with each airplane, and it must contain the following :
(1)
Information required by Secs. 25.1583 through 25.1587.
(2)
Other information that is necessary for safe operation because of design, ope-rating, or handling characteristics.
(3)
[Any limitation, procedure, or other information establishedas a condition of compliance with the applicable noise standards of Part 36 of this chapter.]
(b)
Approved information. Each part of the manual listed in Secs. 25.1583 through 25.1587, that is appropriate to the airplane, must be furnished, veri.ed, and ap-proved, and must be segregated, identi.ed, and clearly distinguished from each unapprovedpart of that manual.
(c)
[Reserved]
(d)
Each Airplane Flight Manual must include a table of contents if the complexity of the manual indicates a need for it.
Amdt. 25-72, E.. 8/20/90
′
Elodie Roux. Septembre 2003
Subpart G : Operating Limitations and Information
FAR 25.1583 : Operating limitations.
(a)
Airspeed limitations. The following airspeed limitations and any other airspeed limi-tations necessary for safe operation must be furnished :
(1)
The maximum operating limit speed VMO/MMO and a statement that this speedlimitmay notbedeliberately exceededinany regimeof .ight(climb, cruise, or descent) unless a higher speed is authorized for .ight test or pilot training.
(2)
If an airspeed limitation is based upon compressibility e.ects, a statement to this e.ect and information as to any symptoms, the probable behavior of the airplane, and the recommended recoveryprocedures.
(3)
The maneuveringspeed VA and a statement thatfull application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, should be con.ned to speeds below this value.
(4)
The .ap extended speed VFE and the pertinent .ap positions and engine po-wers.
(5)
The landing gear operating speed or speeds, and a statement explaining the speeds as de.ned in Sec. 25.1515(a).
(6)
The landing gear extended speed VLE, if greater than VLO, and a statement thatthisisthemaximumspeed at which theairplanecanbesafely.ownwith the landing gear extended.
(b)
Powerplant limitations. The following information must be furnished :
(1)
Limitations required by Sec. 25.1521 and Sec. 25.1522.
(2)
Explanation of the limitations, when appropriate.
(3)
Information necessary for marking the instruments required by Secs. 25.1549 through 25.1553.
(c)
[Weight and loading distribution. The weight and center of gravity limitations esta-blished under Sec. 25.1519 must be furnished in the Airplane Flight Manual. All of thefollowinginformation,including the weightdistributionlimitations established under Sec. 25.1519, must be presented either in the Airplane Flight Manual or in a separate weight and balance control and loading document that is incorporated by reference in the Airplane Flight Manual :
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本文鏈接地址：FAA規章 美國聯邦航空規章 Federal Aviation Regulations 4(41)
