Goto Section: 87.131 | 87.135 | Table of Contents
FCC 87.133
Revised as of October 1, 2013
Goto Year:2012 |
2014
§ 87.133 Frequency stability.
(a) Except as provided in paragraphs (c), (d), (f), and (g) of this
section, the carrier frequency of each station must be maintained
within these tolerances:
Frequency band (lower limit exclusive, upper limit inclusive), and
categories of stations Tolerance ^1 Tolerance ^2
(1) Band-9 to 535 kHz:
Aeronautical stations 100 100
Aircraft stations 200 100
Survival craft stations on 500 kHz 5,000 20 Hz ^3
Radionavigation stations 100 100
(2) Band-1605 to 4000 kHz:
Aeronautical fixed stations:
Power 200 W or less 100 100 ^8
Power above 200 W 50 50 ^8
Aeronautical stations:
Power 200 W or less 100 ^7 100 ^7 8
Power above 200 W 50 ^7 50 ^7 8
Aircraft stations 100 ^7 100 ^7
Survival craft stations on 2182 kHz 200 20 Hz ^3
(3) Band-4 to 29.7 MHz:
Aeronautical fixed stations:
Power 500 W or less 50
Power above 500 W 15
Single-sideband and Independent-sideband emission:
Power 500 W or less 50 Hz
Power above 500 W 20 Hz
Class F1B emissions 10 Hz
Other classes of emission:
Power 500 W or less 20
Power above 500 W 10
Aeronautical stations:
Power 500 W or less ^7 100 100 ^7
Power above 500 W ^7 50 50 ^7
Aircraft stations ^7 100 100 ^7
Survival craft stations on 8364 kHz 200 50 Hz ^3
(4) Band-29.7 to 100 MHz:
Aeronautical fixed stations:
Power 200 W or less 50
Power above 200 W 30
Power 50 W or less 30
Power above 50 W 20
Operational fixed stations:
73-74.6 MHz (Power 50 W or less) 50 30
73-74.6 MHz (Power above 50 W) 20 20
72-73.0 MHz and 75.4-76.0 MHz 5 5
Radionavigation stations 100 50
(5) Band-108 to 137 MHz:
Aeronautical stations ^4 50 ^12 20
Emergency locator transmitter test stations 50 50
Survival craft stations on 121.5 MHz 50 50
Emergency locator stations 50 50
Aircraft and other mobile stations in the Aviation Services ^5 50
^13 30
Radionavigation stations 20 20
Differential GPS 2
(6) Band-137 to 470MHz:
Aeronautical stations 50 20
Survival craft stations on 243 MHz 50 50
Aircraft stations 50 ^5 30 ^10
Radionavigation stations 50 50
Emergency locator transmitters on 406 MHz N/A 5
(7) Band-470 to 2450 MHz:
Aeronautical stations 100 20
Aircraft stations 100 20
Aircraft earth station 320 Hz ^11
Radionavigation stations:
470-960 MHz 500 500
960-1215 MHz 20 20
1215-2450 MHz 500 500
(8) Band-2450 to 10500 MHz:
Radionavigation stations ^6 9 1250 1250 ^6 9
(9) Band-10.5 GHz to 40 GHz:
Radionavigation stations 5000 5000
^1 This tolerance is the maximum permitted until January 1, 1990, for
transmitters installed before January 2, 1985, and used at the same
installation. Tolerance is indicated in parts in 10 ^6unless shown as
Hertz (Hz).
^2 This tolerance is the maximum permitted after January 1, 1985 for
new and replacement transmitters and to all transmitters after January
1, 1990. Tolerance is indicated in parts in 10 ^6unless shown as Hertz
(Hz).
^3 For transmitters first approved after November 30, 1977.
^4 The tolerance for transmitters approved between January 1, 1966, and
January 1, 1974, is 30 parts in 10 ^6. The tolerance for transmitters
approved after January 1, 1974, and stations using offset carrier
techniques is 20 parts in 10 ^6.
^5 The tolerance for transmitters approved after January 1, 1974, is 30
parts in 10 ^6.
^6 In the 5000 to 5250 MHz band, the FAA requires a tolerance of +-10
kHz for Microwave Landing System stations which are to be a part of the
National Airspace System (FAR 171).
^7 For single-sideband transmitters operating in the frequency bands
1605-4000 kHz and 4-29.7 MHz which are allocated exclusively to the
Aeronautical Mobile (R) Service, the tolerance is: Aeronautical
stations, 10 Hz; aircraft stations, 20 Hz.
^8 For single-sideband radiotelephone transmitters the tolerance is: In
the bands 1605-4000 kHz and 4-29.7 MHz for peak envelope powers of 200
W or less and 500 W or less, respectively, 50 Hz; in the bands
1605-4000 kHz and 4-29.7 MHz for peak envelope powers above 200 W and
500 W, respectively, 20 Hz.
^9 Where specific frequencies are not assigned to radar stations, the
bandwidth occupied by the emissions of such stations must be maintained
within the band allocated to the service and the indicated tolerance
does not apply.
^10 Until January 1, 1997, the maximum frequency tolerance for
transmitters with 50 kHz channel spacing installed before January 2,
1985, is 50 parts in 10 ^6.
^11 For purposes of certification, a tolerance of 160 Hz applies to the
reference oscillator of the AES transmitter. This is a bench test.
^12 For emissions G1D and G7D, the tolerance is 2 parts per 10^6.
^13 For emissions G1D and G7D, the tolerance is 5 parts per 10^6.
(b) The power shown in paragraph (a) of this section is the peak
envelope power for single-sideband transmitters and the mean power for
all other transmitters.
(c) For single-sideband transmitters, the tolerance is:
(1) All aeronautical stations on land--10 Hz.
(2) All aircraft stations--20 Hz.
(d) For radar transmitters, except non-pulse signal radio altimeters,
the frequency at which maximum emission occurs must be within the
authorized frequency band and must not be closer than 1.5/T MHz to the
upper and lower limits of the authorized bandwidth, where T is the
pulse duration in microseconds.
(e) The Commission may authorize tolerances other than those specified
in this section upon a satisfactory showing of need.
(f) The carrier frequency tolerance of transmitters operating in the
1435-1535 MHz and 2310-2390 MHz bands manufactured before January 2,
1985, is 0.003 percent. The carrier frequency tolerance of transmitters
operating in the 1435-1535 MHz and 2310-2390 MHz bands manufactured
after January 1, 1985, is 0.002 percent. After January 1, 1990, the
carrier frequency tolerance of all transmitters operating in the
1435-1535 MHz and 2310-2390 MHz bands is 0.002 percent.
(g) Any aeronautical enroute service transmitter operating in U.S.
controlled airspace with 8.33 kHz channel spacing (except equipment
being tested by avionics equipment manufacturers and flight test
stations prior to delivery to their customers for use outside U.S.
controlled airspace) must achieve 0.0005% frequency stability when
operating in that mode.
[ 53 FR 28940 , Aug. 1, 1988, as amended at 56 FR 38084 , Aug. 12, 1991;
57 FR 45749 , Oct. 5, 1992; 58 FR 31027 , May 26, 1993; 63 FR 36607 , July
7, 1998; 64 FR 27474 , May 20, 1999; 66 FR 26799 , May 15, 2001; 69 FR 32880 , June 14, 2004; 76 FR 17350 , Mar. 29, 2011]
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Goto Section: 87.131 | 87.135
Goto Year: 2012 |
2014
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