(2)
Havea reliable,approvedpersonnel carryingdevicesystemthathasthe struc-tural capability and personnel safety features essential for external occupant safety;
(3)
Haveplacards and markings at all appropriatelocationsthat clearly statethe essential system operating instructions and, for the personnel carrying device system, the ingress and egress instructions;
(4)
Have equipment to allowdirectintercommunication amongrequired crewmem-bers and external occupants; and
(5)
Have the appropriate limitations and procedures incorporated in the .ight manual for conducting human external cargo operations.
(d)
The criticallycon.guredjettisonable externalloads mustbe shownby a combination of analysis, ground tests, and .ight tests to be both transportable and releasable throughout the approved operational envelope without hazard to the rotorcraft during normal .ight conditions.Inaddition,these externalloadsmustbeshownto be releasable without hazard to the rotorcraft during emergency .ight conditions.
(e)
A placard or marking must be installed next to the external-load attaching means clearly stating any operational limitations and the maximum authorized external load as demonstrated under Sec. 27.25 and this section.
(f)
The fatigue evaluation of Sec. 27.571 of this part does not apply to rotorcraft-load combinations to be used for nonhuman external cargo except for the failure of critical structural elements that would result in a hazard to the rotorcraft. For rotorcraft-load combinations to be used for human external cargo, the fatigue eva-luation of Sec. 27.571 of this part applies to the entire quick release and personnel carrying device structural systems and their attachments.]
Amdt. 27-36, E.. 10/5/99
′
Elodie Roux. Septembre 2003
Subpart D : Design and Construction
64.9 Miscellaneous
FAR 27.871 : Levelling marks
There must be reference marks for leveling the rotorcraft on the ground.
FAR 27.873 : Ballast provisions
Ballast provisions must be designed and constructed to prevent inadvertent shifting of ballast in .ight.
Chapitre 65 Subpart E : Powerplant
Sommaire
65.1General ............................... 839
FAR27.901:Installation .................... 839
FAR27.903:Engines ...................... 839
FAR27.907:Enginevibration ................. 840
65.2RotorDriveSystem . . . . . . . . . . . . . . . . . . . . . . . . 840 FAR27.917:Design ....................... 840 FAR27.921:Rotorbrake .................... 840 FAR 27.923 : Rotor drive system and control mechanism tests 841 FAR27.927:Additionaltests. . . . . . . . . . . . . . . . . . 842 FAR27.931:Shafting critical speed . . . . . . . . . . . . . . 843 FAR27.935:Shaftingjoints .................. 843 FAR 27.939 : Turbine engine operating characteristics . . . . 843
65.3FuelSystem. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 844 FAR27.951:General ...................... 844 FAR27.952:[Fuel systemcrash resistance.] . . . . . . . . . . 844 FAR 27.953 : Fuel system independence . . . . . . . . . . . . 846 FAR27.954:[Fuel systemlightningprotection.] . . . . . . . 847 FAR27.955:Fuel.ow. . . . . . . . . . . . . . . . . . . . . . 847 FAR27.959:Unusablefuel supply . . . . . . . . . . . . . . . 848 FAR 27.961 : Fuel system hot weather operation . . . . . . . 848 FAR27.963:Fueltanks:general . . . . . . . . . . . . . . . . 848 FAR27.965:[Fueltanktests.] ................. 849 FAR27.967:[Fueltankinstallation.] . . . . . . . . . . . . . . 850 FAR27.969:Fueltank expansionspace . . . . . . . . . . . . 850 FAR27.971:Fueltank sump .................. 851 FAR27.973:Fueltank.llerconnection . . . . . . . . . . . . 851 FAR27.975:Fueltank vents .................. 851 FAR27.977:Fueltank outlet. . . . . . . . . . . . . . . . . . 851
65.4FuelSystemComponents. . . . . . . . . . . . . . . . . . . . . 852 FAR27.991:Fuelpumps .................... 852 FAR 27.993 : Fuel system lines and .ttings . . . . . . . . . . 852 FAR27.995:Fuel valves. . . . . . . . . . . . . . . . . . . . . 852
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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(101)
