75.2RotorDriveSystem .............................. 998

TABLE DES MATI ERES
75.3FuelSystem. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1004
75.4FuelSystemComponents ........................... 1014

75.5OilSystem ................................... 1016

75.6Cooling ..................................... 1020

75.7InductionSystem. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1023
75.8ExhaustSystem. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1026
75.9PowerplantControlsandAccessories . . . . . . . . . . . . . . . . . . . . . 1027 75.10PowerplantFireProtection .......................... 1030
76 Subpart F : Equipment 1037
76.1General ..................................... 1039

76.2Instruments:Installation ........................... 1044

76.3ElectricalSystemsandEquipment . . . . . . . . . . . . . . . . . . . . . . 1048
76.4Lights ...................................... 1052

76.5Safety Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1056
76.6MiscellaneousEquipment ........................... 1058

77 Subpart G : Operating Limitations and Information 1063
77.1Operating Limitations ............................. 1065

77.2MarkingsandPlacards. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1070
77.3RotorcraftFlightManual ........................... 1073

78 Appendix A : Instructions for Continued Airworthiness 1077
79 Appendix B : Airworthiness Criteria for Helicopter Instrument Flight1081
Chapitre 71 Subpart A : General
Sommaire
FAR29.1:Applicability. .................... 916
FAR29.2:[Special retroactiverequirements.] . . . . . . . . . 916

915
Subpart A : General
FAR 29.1 : Applicability.
(a)
This Part prescribes airworthiness standards for the issue of type certi.cates, and changes to those certi.cates, for transport category rotorcraft.

(b)
Transport category rotorcraft must be certi.cated in accordance with either the CategoryA orCategoryB requirementsof thisPart.A multienginerotorcraft may be type certi.cated as both Category A and Category B with appropriate and di.erent operating limitations for each category.

(c)
Rotorcraft with a maximum weight greater than 20,000 pounds and 10 or more passenger seats must be type certi.cated as Category A rotorcraft.

(d)
Rotorcraft with a maximum weight greater than 20,000 pounds and nine or less passenger seats may be type certi.cated as Category B rotorcraft provided in the Category A requirements of Subparts C, D, E, and F of this Part are met.

(e)
[Rotorcraft with a maximum weight of 20,000 pounds or less but with 10 or more passenger seats may be type certi.cated as Category B rotorcraft provided the Category A requirements of Secs. 29.67(a)(2), 29.87, 29.1517, and subparts C, D, E, and F of this part are met.]

(f)
Rotorcraftwith a maximum weight of20,000pounds orless and nine orlesspassenger seats may be type certi.cated as Category B rotorcraft.

(g)
Each person who applies under Part 21 for a certi.cate or change described in paragraphs(a)through(f)ofthis section must show compliance withthe applicable requirements of this Part.

Amdt. 29-39, E.. 6/10/96
FAR29.2:[Specialretroactive requirements.]
[For each rotorcraft manufactured after September 16, 1992, each applicant must show that each occupant’s seat is equipped with a safety belt and shoulder harness that meetsthe requirements ofparagraphs(a),(b), and(c) of this section.
(a)
Each occupant’s seat must have a combined safety belt and shoulder harness with a single-point release. Each pilot’s combined safety belt and shoulder harness must allow eachpilot, when seated with safetybelt and shoulderharnessfastened, toper-form all functions necessary for .ight operations. There must be a means to secure belts andharnesses, when notin use,topreventinterference with the operation of the rotorcraft and with rapid egress in an emergency.
　
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