Secondary Surveillance Radar (SSR) is a secondary radar system: instead of relying on echoes, the ground station interrogates airborne transponders which transmit their own coded replies. This gives much more information than primary radar.
📡 SSR Advantages Over Primary Radar
Identity (callsign equivalent code)
Altitude (Mode C, no need for R/T)
Strong, reliable signal (transponder active transmitter, not a passive reflector)
Works regardless of aircraft size or material (no 4th power law limitation)
Not affected by weather, ground clutter or sea return
Mode S: Data link — downlinked aircraft data; uplinked ATC messages
Fig 14.1 & 14.2: SSR antenna (rotates with primary head) and overall principle of operation
2. Ground Equipment
📡 SSR Ground Station
Parameter
Detail
Transmit frequency
1030 MHz (UHF)
Receive frequency
1090 MHz (UHF)
Antenna type
Mounted on top of primary radar antenna; co-rotates
Antenna beam
Narrow in azimuth (1–3°)
SLS (Side Lobe Suppression)
Omnidirectional pulse P2 transmitted simultaneously with P1; if transponder sees P2 > P1, it suppresses reply → prevents side-lobe interrogations
Processor
Decodes replies, displays on PPI alongside primary return
3. Airborne Transponder
Fig 14.3: Transponder control panel — STBY, ON, ALT, IDENT positions, mode selector, code display
📡 Transponder Operation
Parameter
Detail
Receive frequency
1030 MHz
Transmit frequency
1090 MHz
Reply delay
50 µs (transponder receives and delays before replying, to allow distance measurement)
Antenna
Omni-directional (top and bottom fuselage)
STANDBY
System active, will NOT respond to interrogations (used on ground when not required)
ON
Mode A (identity) only
ALT
Mode C (altitude encoding) + Mode A
IDENT / SPI
Special Position Identification pulse — flashes radar blip for 20 seconds
4. Interrogation Modes
Fig 14.4: Pulse spacings for Mode A (8 µs) and Mode C (21 µs) | Fig 14.5: Reply pulse train (F1...SPI...F2)
📡 Mode Comparison
Mode
P1–P3 Spacing
Reply Contains
Info Provided
A (Identity)
8 µs
4096 identity codes
Aircraft identity (4-digit squawk)
B
17 µs
Identity codes
Aircraft identity (alternate)
C (Altitude)
21 µs
Altitude in 100 ft increments
Pressure altitude (re: 1013.25 hPa)
D
25 µs
Future use
—
⚡ Key Mode Details
Mode A provides 4096 identity codes (0000–7777 octal, with 1200, 7000, 7700 reserved/restricted)
Mode C altitude: encoded in 100 ft increments using Gillham code; referenced to 1013.25 hPa regardless of QNH set
Mode C displayed separately on PPI — ATC can read altitude without R/T
Transponder replies with framing pulses F1, F2 spaced 20.3 µs, with information pulses between
⚠ Required Actions
When ATC say “SQUAWK IDENT”: press IDENT button → SPI for 20 seconds
HIJACK: squawk 7500
Loss of R/T: squawk 7600
Emergency: squawk 7700
Military conspicuity: squawk 7000
VFR conspicuity (no ATC unit): squawk 7000
5. Transponder Codes
Fig 14.6: Reply codes — 4096 combinations of 4 digits 0-7 in Mode A
📡 Code Summary
Code
Meaning
7700
Emergency
7600
Radio failure
7500
Unlawful interference (hijack)
7000
Military conspicuity / VFR conspicuity (UK)
2000
Entering controlled airspace without ATC clearance
Assigned
Four-digit code assigned by ATC
6. SSR Problems
Fig 14.7: Garbling (two aircraft within 1.7 NM cause overlapping replies) and Fruiting (random interrogations cause interference)
⚠ Garbling
Two aircraft within 1.7 NM of each other appear to be in the same direction from the ground station
Their replies overlap → garbled, unreadable replies
Solution: Mode S (selective addressing)
⚠ Fruiting (Phantoms)
Multiple ground interrogators on same frequency
Transponder receives interrogation from station B but reply is picked up by station A
Station A sees a phantom target at incorrect position
Solution: ISLS (Improved Side Lobe Suppression) — synchronised interrogation timing between stations
7. Mode S
✓ Mode S Key Features
Feature
Detail
Addressing
Each aircraft has a unique 24-bit address (16.7 million combinations)
Selective interrogation
Ground station interrogates ONLY the target aircraft → eliminates garbling
Data link
Bidirectional: aircraft can downlink data; ATC can uplink instructions
Altitude resolution
25 ft (vs 100 ft for Mode C)
ACAS / TCAS
Uses Mode S for aircraft-to-aircraft interrogation to provide collision avoidance
Automatic Dependent Surveillance Broadcast — squitter every 0.5 s; position via GPS
8. SSR Summary
Parameter
Detail
Type
Secondary radar; interrogation–reply
Ground Tx
1030 MHz (UHF)
Transponder Tx
1090 MHz (UHF)
Transponder delay
50 µs
Mode A spacing
8 µs → 4096 codes → identity
Mode C spacing
21 µs → pressure altitude re 1013.25 hPa → 100 ft increments
SPI
IDENT pressed → 20 s enhanced blip
Garbling
<1.7 NM separation → overlapping replies
Fruiting
Phantom returns from multiple interrogators
Mode S address
24 bits → 16.7 million unique addresses
Mode S altitude
25 ft resolution
9. Practice Questions
Q1. SSR operates on frequencies:
(a) 1030 MHz ground Tx, 1090 MHz airborne Tx
(b) 1090 MHz ground Tx, 1030 MHz airborne Tx
(c) 9375 MHz both
(d) 960 MHz both
Answer: (a) Ground transmits at 1030 MHz, airborne transponder replies at 1090 MHz.
Q2. Mode C provides ATC with:
(a) aircraft callsign
(b) airspeed
(c) position
(d) pressure altitude
Answer: (d) Mode C (P1–P3 spacing = 21 µs) provides pressure altitude referenced to 1013.25 hPa in 100 ft increments.
Q3. Advantage of Mode S over Mode A/C:
(a) no transponder required
(b) not dependent on pressure altimeter
(c) eliminates garbling by selective addressing
(d) uses VHF frequencies
Answer: (d) Mode S eliminates garbling through selective addressing — each aircraft has a unique 24-bit ICAO address; ground station interrogates only one aircraft at a time.
Answer: (c) Mode S uses a 24-bit ICAO address, providing up to 16.7 million unique aircraft identifiers, enabling selective interrogation and data link capability.
DGCA CPL/ATPL Radio Navigation Study Notes
Chapter 14 — SSR (Secondary Surveillance Radar) Capt Pankaj Pahil | www.ghostaviator.com For personal study use only.