18.3 Aircraft Antennas, Frequencies & Equipment Functions
Key Takeaways
- Aircraft VHF communications operate about 118.000–136.975 MHz (pool notes worldwide extension up to ~151.975 MHz)
- ELTs transmit on 121.5, 243, and 406 MHz; radio altimeters operate about 4250–4350 MHz; Mode C/S L-band blades serve 1030/1090 MHz
- VOR/LOC antennas are horizontally polarized omnidirectional receive antennas; marker beacons use balanced loop receive antennas; transponders use L-band monopole blades
- Aircraft often use 400 Hz prime power so transformers, chokes, and filters can be smaller and lighter than 60 Hz designs
- GROL function IDs include dynamic microphones, typical HF ~100 W vs VHF ~20 W RF output, SELCAL selective calling, and clearing the radar beam path before ground RADAR tests
18.3 Aircraft Antennas, Frequencies & Equipment Functions
Quick Answer: VHF COM ≈ 118.000–136.975 MHz (pool: worldwide up to ~151.975 MHz). ELT: 121.5, 243, and 406 MHz. Radio altimeter ≈ 4250–4350 MHz. VOR/LOC antenna = horizontally polarized omnidirectional receive; marker beacon = balanced loop receive; Mode C = L-band monopole blade omni. 400 Hz aircraft power → magnetic parts smaller/lighter. Mics mostly dynamic; typical airborne HF ≈ 100 W, VHF ≈ 20 W. SELCAL lets ground call a selected aircraft without constant monitoring. Before ground-testing RADAR, clear personnel from the antenna beam.
Key topics 072 (Aircraft Antenna Systems and Frequencies) and 073 (Equipment Functions) are identification-heavy: match the box, the antenna, and the frequency—and know a few operational safety/function facts that show up verbatim on Element 3.
Master frequency map (civil aircraft RF)
| System | Approx. frequency | Antenna / notes |
|---|---|---|
| ADF / NDB receive | 190–1750 kHz | Loop + sense |
| Marker beacon | 75 MHz | Balanced loop receive |
| VOR | 108.00–117.95 MHz | Horiz. polarized omni receive |
| Localizer | 108.10–111.95 MHz | Same NAV antenna family as VOR/LOC |
| VHF COM | 118.000–136.975 MHz (worldwide up to ~151.975 MHz) | Vertical blade / whip |
| ELT | 121.5, 243, and 406 MHz | Dedicated ELT antenna; G-switch activation |
| Glideslope | ~329.15–335.00 MHz | Folded dipole receive |
| DME | 962–1213 MHz | L-band blade |
| Transponder / ATCRBS | RX 1030 / TX 1090 MHz | L-band monopole blade omni |
| TCAS interrogations (Mode S PPM) | 1030 MHz directional from TCAS antenna pattern | Phased/directional on aircraft TCAS |
| Radio (radar) altimeter | 4250–4350 MHz | Paired TX/RX antennas on belly |
Memorize the clusters: LF–MF (ADF), VHF NAV (108–118), VHF COM (118–137), UHF glideslope (~330), L-band DME/XPDR (~1 GHz), C-band radio altimeter (~4.3 GHz).
VHF communications band
Element 3 states the frequency range of an aircraft’s Very High Frequency (VHF) communications as 118.000 MHz to 136.975 MHz (worldwide up to 151.975 MHz). Do not assign the 108–118 MHz NAV band to voice COM, or the 329–335 MHz glideslope band to tower frequencies. Spacing has tightened over decades (25 kHz → 8.33 kHz in many regions), but the band edges are what the pool tests.
VHF COM is essentially line-of-sight; altitude helps range. Antennas are typically vertically polarized blades or whips mounted for a clear view and a solid RF ground plane (airframe skin).
Emergency Locator Transmitters (ELT)
Aircraft ELTs operate on 121.5, 243, and 406 MHz (pool wording includes all three). Roles:
| Frequency | Role |
|---|---|
| 121.5 MHz | Civil VHF distress / legacy homing (satellite monitoring of 121.5 ended; still used for local aural homing) |
| 243 MHz | Military UHF distress / legacy |
| 406 MHz | Digital COSPAS-SARSAT beacon with coded identity (and usually GPS position on modern units) |
An ELT automatically activates on crash impact (G-switch) or can be armed manually, transmitting a distress signal to aid search and rescue. Registration of 406 MHz beacons and correct antenna mounting are maintenance/compliance items—not optional accessories.
Radio altimeter frequencies
The frequency range of an aircraft’s radio altimeter on Element 3 is 4250 MHz to 4350 MHz (~4.3 GHz C-band). Radio altimeters measure height above terrain (AGL), not pressure altitude MSL. They typically use FM-CW or similar ranging on belly antennas. Do not confuse:
- 121.5 MHz → ELT/distress, not radio alt
- 1090 MHz → transponder replies, not radio alt
- 9 GHz-class → weather/marine X-band radar territory, not the civil radio-alt pool answer
Antenna types the pool names explicitly
VOR and localizer
What type of antenna is used in an aircraft’s VOR and Localizer (LOC) installations? A horizontally polarized omnidirectional reception antenna. VOR/LOC ground signals are horizontally polarized; the airborne antenna is receive-oriented for that polarization with broad azimuth coverage so course deviation works through turns.
Marker beacon
ILS marker beacon installation: a balanced loop reception antenna. Loop geometry favors the overhead marker radiation pattern as the aircraft passes through the beacon’s “football” of energy.
Mode C / ATCRBS
Antenna attached to a Mode C transponder installation to receive 1030 MHz interrogations: an L-band monopole blade-type omnidirectional antenna. Blades are low-drag, broadband enough for 1030/1090 MHz, and nearly omnidirectional in azimuth when mounted on a proper ground plane.
TCAS / Mode S interrogation pattern (ground-station side of the item)
When a ground station phased-array directional antenna transmits the PPM pulses in a Mode S interrogation of an aircraft’s TCAS installation context on the pool, the pattern called out is a 1030 MHz directional pattern. (Aircraft reply on 1090 MHz; keep the uplink/downlink directions straight.)
Glideslope (recap)
As in 18.2: glideslope receive antenna is typically a folded dipole reception antenna.
Placement, drag, ground plane, and isolation
Aircraft antennas are a compromise among RF performance, aerodynamic drag, structural integrity, and EMC isolation:
| Concern | Why it matters to GROL work |
|---|---|
| Ground plane | Blade/monopole impedance and pattern assume conductive skin; composite airframes need designed ground planes or doublers |
| Drag / location | Prefer blades over long wires; keep clear of control surfaces and other antennas’ near fields |
| Isolation | Separate TX antennas (COM, ELT, XPDR, DME) so simultaneous transmissions do not desense receivers |
| Polarization match | Horizontal for VOR/LOC/GS; vertical for COM/XPDR blades; wrong polarization = weak signal with “good” coax |
| Lightning / bonding | Proper bonding straps and static wicks reduce noise and damage paths |
| Duplicate systems | Transport aircraft may have upper and lower XPDR antennas for attitude coverage |
When diagnosing “weak VOR” or “no Mode C,” walk the antenna → connector → coax → LRU path before swapping expensive boxes. Corrosion at BNC/TNC connectors and crushed coax under floorboards are classic finds.
Equipment functions (3-K-073)
400 Hz aircraft power
Some aircraft and avionics operate with a prime power line frequency of 400 Hz. The principle advantage of a higher line frequency: the magnetic devices in a 400 Hz power supply such as transformers, chokes and filters are smaller and lighter than those used in 60 Hz power supplies. Weight and volume dominate aerospace design; higher frequency allows less iron/core for the same reactance. Pool distractors about “always draws less current,” “always more efficient/cooler,” or “much cheaper” miss the size/weight rationale.
Microphones
Aviation services use predominantly dynamic microphones. Carbon, condenser, and piezoelectric types appear in other niches; the Element 3 expected word is dynamic.
HF vs VHF transmitter power
Typical airborne HF transmitters usually provide a nominal RF power output to the antenna of about 100 watts, compared with about 20 watts RF output from a typical VHF transmitter (100, 20 on the pool). HF must close longer sky-wave/ground-wave paths; VHF COM is short-range line-of-sight with good antennas and altitude.
Ground-testing aircraft RADAR
Before ground testing an aircraft RADAR, the operator should ensure that the area in front of the antenna is clear of other maintenance personnel to avoid radiation hazards. High-power microwave energy can injure tissue and ignite hazards; hangar procedure is “beam path clear” first—not merely “measure supply voltages” or “shield the receiver.”
SELCAL
SELCAL (Selective Calling) is a type of aircraft communications system where a ground-based transmitter can call a selected aircraft or group of aircraft without the flight crew monitoring the ground-station frequency continuously. HF oceanic flights use SELCAL so crews are not locked to a noisy HF channel full-time; a chime alerts them when their code is sent. It is not encryption, continuous selectivity calibration, or airborne distance calculation.
Function-identification drill for techs
| Symptom or task | Likely system |
|---|---|
| No left/right CDI on ILS frequency | Localizer / VOR-LOC antenna / NAV RX |
| No up/down needles, CDI works | Glideslope RX / folded-dipole antenna / pairing |
| No blue/amber/white marker lights | Marker RX / balanced loop / 75 MHz path |
| No distance on VOR frequency | DME interrogator / L-band antenna / pairing |
| ATC has no altitude | Mode C encoder path / 1090 reply / blade antenna |
| No COM with tower | VHF COM 118–137 MHz / vertical antenna |
| Beacon not heard after hard landing | ELT 121.5/243/406 / G-switch / ELT antenna |
| Height AGL disagree with chart | Radio altimeter 4250–4350 MHz antennas |
| Crew wants hands-off HF watch | SELCAL installation |
Exam-day checklist (3-K 072–073)
- VHF COM 118.000–136.975 MHz (up to ~151.975 worldwide note).
- ELT 121.5, 243, and 406 MHz; radio altimeter 4250–4350 MHz.
- VOR/LOC antenna = horizontally polarized omni receive; marker = balanced loop; Mode C = L-band blade omni; TCAS/Mode S ground interrogation pattern item → 1030 MHz directional.
- 400 Hz → smaller/lighter magnetic components.
- Mics dynamic; HF ~100 W vs VHF ~20 W; SELCAL = selective ground call without continuous monitoring.
- Ground RADAR test → clear people from the antenna beam first.
Topic 3-K is complete when you can name each aircraft radio navigation and surveillance system, its frequency band, its antenna class, and the one-sentence function Element 3 expects—then move on to installation, maintenance, and repair instruments in the next chapter cluster (3-L).
What is the frequency range of aircraft VHF communications on Element 3, and on which frequencies do aircraft ELTs operate?
What antenna types are used for aircraft VOR/LOC installations, ILS marker beacon installations, and Mode C transponder 1030 MHz reception?
What is the Element 3 frequency range of an aircraft radio altimeter, and what is the principle advantage of 400 Hz prime power on aircraft?
Aviation services predominantly use what microphone type; what typical RF outputs do airborne HF and VHF transmitters provide; what is SELCAL; and what must you do before ground-testing aircraft RADAR?