Amdt. 23-34, E.. 2/17/87
FAR 23.865 : Fire protection of .ight controls, engine mounts, and other .ight structure.
[Flight controls, engine mounts, andother .ight structure located in designated .re zones,orinadjacent areasthatwouldbesubjected tothee.ectsof .reinthedesignated .re zones, must be constructed of .reproof material or be shielded so that they are capable of withstanding the e.ects of a .re. Engine vibration isolators must incorporate suitablefeaturesto ensurethatthe engineis retainedif the non-.reproofportionsof the isolators deteriorate from the e.ects of a .re.] Amdt. 23-48, E.. 03/11/96
31.9 Electrical Bonding and Lightning Protection
FAR23.867:[Electricalbonding andprotectionagainstlightning and static electricity.]
(a)
The airplane must be protected against catastrophic e.ects from lightning.

(b)
For metallic components, compliance with paragraph (a) of this section may be shown by–

(1)
Bonding the components properly to the airframe; or

(2)
Designing the components so that a strike will not endanger the airplane.

(c)
For non-metallic components, compliance withparagraph(a) of this section may be shown by–

(1)
Designing the components to minimize the e.ect of a strike; or

(2)
Incorporating acceptable means of diverting the resulting electrical current so as not to endanger the airplane.

Amdt. 23-49, E.. 03/11/96
31.10 Miscellaneous
FAR23.871 :[Leveling means.]
[There mustbe meansfordeterminingwhenthe airplaneisin alevelposition onthe ground.] Amdt. 23-7, E.. 09/14/69
′
Elodie Roux. Septembre 2003
Subpart D : Design and Construction
Chapitre 32 Subpart E : Powerplant
Sommaire
32.1General ............................... 352

FAR23.901:Installation. .................... 352 FAR23.903:Engines. ...................... 352 FAR23.904:[Automaticpowerreservesystem.] . . . . . . . 354 FAR23.905:Propellers.. . . . . . . . . . . . . . . . . . . . . 354 FAR23.907:Propellervibration. . . . . . . . . . . . . . . . . 355 FAR23.909:[Turbochargersystems.] . . . . . . . . . . . . . 355 FAR23.925:Propellerclearance. . . . . . . . . . . . . . . . . 356 FAR 23.929 : Engine installation ice protection. . . . . . . . . 356 FAR23.933:Reversing systems. . . . . . . . . . . . . . . . . 356 FAR 23.934 : [Turbojet and turbofan engine thrust reverser systemstests.] ..................... 357 FAR 23.937 : Turbopropeller-drag limiting systems. . . . . . 357 FAR 23.939 : Powerplant operating characteristics. . . . . . . 358 FAR23.943:Negativeacceleration. . . . . . . . . . . . . . . 358
32.2FuelSystem. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 358
FAR23.951:General. ...................... 358 FAR 23.953 : Fuel system independence. . . . . . . . . . . . . 358 FAR23.954:[Fuel systemlightningprotection.] . . . . . . . 359 FAR23.955:Fuel.ow. ..................... 359 FAR 23.957 : Flow between interconnected tanks. . . . . . . . 361 FAR23.959:Unusablefuel supply. . . . . . . . . . . . . . . . 361 FAR 23.961 : Fuel system hot weather operation. . . . . . . . 361 FAR23.963:Fueltanks:general. . . . . . . . . . . . . . . . 361 FAR23.965:Fueltanktests. .................. 362 FAR23.967:Fueltankinstallation. . . . . . . . . . . . . . . 363 FAR23.969:Fueltank expansionspace. . . . . . . . . . . . . 364 FAR23.971:Fueltank sump.. . . . . . . . . . . . . . . . . . 364 FAR 23.973 : Fuel tank .ller connection. . . . . . . . . . . . . 364 FAR 23.975 : Fuel tank vents and carburetor vapor vents. . . 365 FAR23.977:Fueltank outlet. ................. 365 FAR23.979:Pressurefueling systems. . . . . . . . . . . . . . 366
349
Subpart E : Powerplant
32.3FuelSystemComponents. . . . . . . . . . . . . . . . . . . . . 366 FAR23.991:Fuelpumps. . . . . . . . . . . . . . . . . . . . . 366 FAR 23.993 : Fuel system lines and .ttings. . . . . . . . . . . 367 FAR23.994:Fuel systemcomponents. . . . . . . . . . . . . . 367 FAR23.995:Fuel valvesand controls. . . . . . . . . . . . . . 367 FAR23.997:Fuel straineror.lter.. . . . . . . . . . . . . . . 368 FAR23.999:Fuel systemdrains. . . . . . . . . . . . . . . . . 368 FAR23.1001:Fueljettisoning system. . . . . . . . . . . . . . 369
　
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