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(iv) Has a means to verify proper operation of the system or device.]
(b) For category A rotorcraft–
(1) An individual oilpressureindicatorfor each engine, and either anindependent warningdevicefor each engine or a master warningdevicefor the engines with means for isolating the individual warning circuit from the master warning device; and
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Elodie Roux. Septembre 2003
Subpart F : Equipment
(2)
An independent fuel pressure warning device for each engine or a master war-ning device for all engines with provision for isolating the individual warning device from the master warning device;

(3)
Fire warning indictors.

(c)
For category B rotorcraft–

(1) Anindividual oilpressureindicatorfor each engine; and

(2)
Fire warning indicators, when .re detection is required. Amdt. 29-40, E.. 8/8/96

FAR 29.1307 : Miscellaneous equipment.
The following is required miscellaneous equipment :
(a)
An approved seat for each occupant.

(b)
A master switch arrangement for electrical circuits other than ignition.

(c)
Hand .re extinguishers.

(d)
A windshield wiper or equivalent device for each pilot station.

(e)
A two-way radio communication system. Amdt. 29-12, E.. 2/1/77

FAR 29.1309 : Equipment, systems, and installations.

(a)
The equipment, systems, andinstallations whosefunctioningis requiredby this sub-chapter mustbedesigned andinstalled to ensurethattheyperformtheirintended functions under any foreseeable operating condition.

(b)
The rotorcraft systems and associated components, considered separately and in relation to other systems, must be designed so that–

(1)
For Category B rotorcraft, the equipment, systems, and installations must be designed topreventhazardstothe rotorcraftif they malfunction orfail; or

(2)
For Category A rotorcraft–

(i)
The occurrence ofanyfailure condition which wouldpreventthe continued safe .ight and landing of the rotorcraft is extremely improbable; and

(ii)
The occurrence of any other failure conditions which would reduce the capability of the rotorcraft or the ability of the crew to cope with adverse operating conditions is improbable.

 

 

(c)
Warning information must be provided to alert the crew to unsafe system opera-ting conditions and to enable them to take appropriate corrective action. Systems, controls, and associated monitoring and warning means must be designed to mini-mize crew errors which could create additional hazards.

(d)
Compliance with the requirements ofparagraph(b)(2) of this section mustbe shown by analysisand,wherenecessary,by appropriateground, .ight,orsimulatortests. The analysis must consider–

(1)
Possible modes of failure, including malfunctions and damage from external sources;

(2)
The probability of multiple failures and undetected failures;

 

(3)
The resulting e.ects on the rotorcraft and occupants, considering the stage of .ight and operating conditions; and

(4)
Thecrewwarning cues,correctiveactionrequired,and the capability ofdetec-ting faults.

(e)
For Category A rotorcraft, each installation whose functioning is required by this subchapter and which requires a power supply is an ”essential load” on the power supply. The power sources and the system must be able to supply the following power loads in probable operating combinations and for probable durations :

(1)
Loads connected to the system with the system functioning normally.

(2)
Essentialloads, afterfailure ofany oneprime mover,power converter, or energy storage device.

(3)
Essential loads, after failure of–

(i)
Any one engine, on rotorcraft with two engines; and
　
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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(88)