FAR29.1411:General. .................. 1056 FAR 29.1413 : Safety belts : passenger warning device. . 1057 FAR 29.1415 : Ditching equipment. . . . . . . . . . . . . 1057 FAR29.1419:[Iceprotection.] . . . . . . . . . . . . . . 1057
76.6MiscellaneousEquipment. . . . . . . . . . . . . . . . . 1058
FAR 29.1431 : Electronic equipment. . . . . . . . . . . . 1058 FAR29.1433:Vacuumsystems. . . . . . . . . . . . . . 1058 FAR29.1435:Hydraulicsystems. . . . . . . . . . . . . 1058 FAR 29.1439 : Protective breathing equipment. . . . . . 1059 FAR29.1457:[Cockpitvoicerecorders.] . . . . . . . . . 1059 FAR29.1459:[Flightrecorder.] . . . . . . . . . . . . . . 1061 FAR29.1461:[Equipment containing high energy rotors.]1062
76.1 General
FAR 29.1301 : Function and installation.
Each item of installed equipment must–
(a)
Be of akind anddesign appropriatetoitsintendedfunction;

(b)
Be labeled as to its identi.cation, function, or operating limitations, or any applicable combination of these factors;

(c)
Beinstalled according tolimitations speci.edforthat equipment; and

(d)
Function properly when installed.

FAR 29.1303 : Flight and navigation instruments.
The following are required .ight and navigational instruments :
(a)
[an airspeed indicator. For CategoryA rotorcraft with VNE less than a speed at which unmistakable pilot cues provide overspeed warning, a maximum al-lowable airspeed indicator must be provided. If maximum allowable airspeed varies with weight, altitude, temperature, or r.p.m., the indicator must show that variation.]

(b)
A sensitive altimeter.

(c)
A magnetic direction indictor.

(d)
A clock displaying hours, minutes, and seconds with a sweep-second pointer or digital presentation.

(e)
A free-air temperature indicator.

(f)
A non-tumbling gyroscopic bank and pitch indicator.

(g)
Agyroscopicrate-of-turnindicatorcombined with anintegral slip-skidindica-tor(turn-and-bankindicator) except only a slip-skidindicatoris required on rotorcraft with a third attitude instrument system that–

(1)
Is usable through .ight attitudes of ± 80 degrees of pitch and ± 120 degrees of roll;

(2)
Ispoweredfrom a sourceindependent of the electricalgenerating system;

(3)
Continues reliable operation for a minimum of 30 minutes after total failure of the electricalgenerating system;

(4)
Operates independently of any other attitude indicating system;

(5)
Is operative withoutselection aftertotalfailure ofthe electricalgenerating system;

(6)
Islocated ontheinstrumentpanelin aposition acceptabletotheAdmi-nistrator that will makeitplainly visible to and usable by anypilot athis station; and

(7)
Is appropriately lighted during all phases of operation.

(h)
A gyroscopic direction indicator.

(i)
A rate-of-climb(vertical speed) indicator.

′
Elodie Roux. Septembre 2003
Subpart F : Equipment
(j) [For Category Arotorcraft, a speed warning device when VNE is less than the speed at which unmistakable overspeed warning is provided by other pilot cues. The speed warningdevice mustgive e.ective aural warning(di.ering distinctively from aural warningsusedfor otherpurposes) tothepilots whenevertheindicated speed exceeds VNE plus 3 knots and must operate satisfactorily throughout the approved range of altitudes and temperatures.]
Amdt. 29-24, E.. 12/6/84
FAR 29.1305 : Powerplant instruments.
The following are required powerplant instruments :
(a) For each rotorcraft–
(1)
A carburetor airtemperatureindicatorfor each reciprocating engine;

(2)
A cylinder head temperature indicator for each air-cooled reciprocating en-gine, and a coolant temperature indicator for each liquid-cooled reciprocating engine;
　
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本文鏈接地址：FAA規章 美國聯邦航空規章 Federal Aviation Regulations 5(86)