background image

818 

14 CFR Ch. I (1–1–19 Edition) 

Pt. 36, App. H 

(i) The beginning of the approach profile is 

represented by helicopter position E. The po-
sition of the helicopter is recorded for a suf-
ficient distance (EK) to ensure recording of 
the entire interval during which the meas-
ured helicopter noise level is within 10 dB of 
Maximum Tone Corrected Perceived Noise 
Level (PNLTM). The reference flight path, 
E

r

K

r

represents a stable flight condition in 

terms of torque, rpm, indicated airspeed, and 
rate of descent resulting in a 6

° 

approach 

angle. 

(ii) The test approach profile is defined by 

the approach angle 

passing directly over 

the station A at a height of AH, to position 
K, which terminates the approach noise cer-
tification profile. The test approach angle 

must be between 5.5

° 

and 6.5

°

(2) The helicopter approaches position H 

along a constant 6

° 

approach slope through-

out the 10 dB down time period. The heli-
copter crosses position E and proceeds along 
the approach slope crossing over station A 
until it reaches position K. 

Section H36.5 Symbols and units. 

The fol-

lowing symbols and units as used in this ap-
pendix for helicopter noise certification have 
the following meanings. 

F

LIGHT

P

ROFILE

I

DENTIFICATION

—P

OSITIONS

 

Posi-

tion 

Description 

A .....

Location of the noise measuring point at the flight- 

track noise measuring station vertically below the 
reference (takeoff, flyover, or approach) flight path. 

C .....

Start of noise certification takeoff flight path. 

C

r

....

Start of noise certification reference takeoff flight path. 

D .....

Start of noise certification flyover flight path. 

D

r

....

Start of noise certification reference flyover path. 

E .....

Start of noise certification approach flight path. 

E

r

....

Start of noise certification reference approach flight 

path. 

F .....

Position on takeoff flight path directly above noise 

measuring station A. 

F

r

....

Position on reference takeoff path directly above 

noise measuring Station A. 

G .....

Position on flyover flight path directly above noise 

measuring station A. 

G

r

....

Position on reference flyover path directly above 

noise measuring Station A. 

H .....

Position on approach flight path directly above noise 

measuring station A. 

H

r

....

Position on reference path directly above noise meas-

uring Station A. 

I ......

End of noise type certification takeoff flight path. 

I

r

.....

End of noise type certification reference takeoff flight 

path. 

J ......

End of noise type certification flyover flight path. 

J

r

.....

End of noise type certification reference flyover flight 

path. 

K .....

End of noise certification approach type flight path. 

K

r

....

End of noise type certification reference approach 

flight path. 

L .....

Position on measured takeoff flight path cor-

responding to PNLTM at station A. 

L

r

....

Position on reference takeoff flight path corresponding 

to PNLTM of station A. 

M ....

Position on measured flyover flight path cor-

responding to PNLTM of station A. 

F

LIGHT

P

ROFILE

I

DENTIFICATION

—P

OSITIONS

— 

Continued 

Posi-

tion 

Description 

M

r

...

Position on reference flyover flight path corresponding 

to PNLTM of station A. 

N .....

Position on measured approach flight path cor-

responding to PNLTM at station A. 

N

r

....

Position on reference approach flight path cor-

responding to PNLTM at station A. 

S .....

Sideline noise measuring station (note: a subscript 

denotes the aircraft orientation relative to the direc-
tion of flight). 

F

LIGHT

P

ROFILE

D

ISTANCES

 

Dis-

tance 

Unit Meaning 

AF .....

Feet 

Takeoff Height. 

The vertical distance be-

tween helicopter and station A. 

AG .....

Feet 

Flyover Height. 

The vertical distance be-

tween the helicopter and station A. 

AH .....

Feet 

Approach Height. 

The vertical distance be-

tween the helicopter and station A. 

AL .....

Feet 

Measured Takeoff Noise Path. 

The distance 

from station A to the measured helicopter 
position L. 

AL

r

....

Feet 

Reference Takeoff Noise Path. 

The distance 

from station A to the reference helicopter 
position L

r

AM ....

Feet 

Measured Flyover Noise Path. 

The distance 

from station A to the measured helicopter 
position M. 

AM

r

...

Feet 

Reference Flyover Noise Path. 

The distance 

from station A to helicopter position M

r

on 

the reference flyover flight path. 

AN .....

Feet 

Measured Approach Noise Path. 

The dis-

tance from station A to the measured heli-
copter noise position N. 

AN

r

....

Feet 

Reference Approach Noise Path. 

The dis-

tance from station A to the reference heli-
copter position N

r

CI ......

Feet 

Takeoff Flight Path Distance. 

The distance 

from position C at which the helicopter es-
tablishes a constant climb angle on the 
takeoff flight path passing over station A 
and continuing to position I at which the 
position of the helicopter need no longer 
be recorded. 

DJ .....

Feet 

Flyover Flight Path Distance. 

The distance 

from position D at which the helicopter is 
established on the flyover flight path pass-
ing over station A and continuing to posi-
tion J at which the position of the heli-
copter need no longer be recorded. 

EK .....

Feet 

Approach Flight Path Distance. 

The distance 

from position E at which the helicopter es-
tablishes a constant angle on the approach 
flight path passing over station A and con-
tinuing to position K at which the position 
of the helicopter need no longer be re-
corded. 

PART B

NOISE MEASUREMENT UNDER

§ 36.801 

Section H36.101 Noise certification test and 

measurement conditions. 

(a) 

General. 

This section prescribes the con-

ditions under which aircraft noise certifi-
cation tests must be conducted and the 

VerDate Sep<11>2014 

12:50 Apr 30, 2019

Jkt 247046

PO 00000

Frm 00828

Fmt 8010

Sfmt 8002

Y:\SGML\247046.XXX

247046

spaschal on DSK3GDR082PROD with CFR