5. CMS – Countermeasures Management Switch

5.1 Concept

The Countermeasures Management Switch (CMS) is a four-way hat switch mounted on the side-stick controller. It controls the aircraft's defensive avionics:

  • ALE-47 CMDS (Countermeasures Dispenser Set) — the chaff and flare dispensing system; and
  • ECM (Electronic Countermeasures) — the radar-jamming system.

ECM configuration depends on block and variant: either external pods (ALQ-131/ALQ-184) or internal avionics (IDIAS).

CMS actuation procedures are presented in Section 5.2 and block and variant differences in Section 5.3.

For complete CMDS (including chaff and flare dispensing programs) and ECM operation, see Dash-34 §§ 2.7.1 and 2.7.2, respectively. Diagrams of the side-stick controller and throttle functions are provided in Dash-34 § 2.1.5. The figure below shows the CMS location on the F-16 side-stick controller.

F-16 Throttle and Side-Stick Controller

Image by Falconpedia (falcon4.wikidot.com), via Wikimedia Commons, licensed under CC BY-SA 3.0.

5.2 CMS Actuation

The tables below cover CMS actuation organized by system: CMDS (Manual, Automatic, Semi-Automatic, Bypass, and Standby modes) and ECM (external pods ALQ-131/ALQ-184 and internal IDIAS).

All CMS actuation described in this chapter is independent of the Master Mode (NAV, A-A or A-G) selected.

Table columns are defined as follows:

  • Mode: The operational context (Master Mode).
  • Direction: CMS hat direction (Up, Down, Left, Right).
  • Action: Press type (Short, Long, Long Hold).
  • Function: What the CMS command activates or controls.
  • Effect / Nuance: Resulting system behavior, including tactics and constraints.
  • Dash34: Reference section in the Dash-34 manual.
  • Training: Recommended BMS training mission(s) (see the BMS Training Manual for descriptions).

5.2.1 CMDS

The ALE-47 CMDS operates in five modes selected via the CMDS CCU MODE knob: Manual (MAN), Automatic (AUTO), Semi-Automatic (SEMI), Bypass (BYP), and Standby (STBY).

The chaff and flare dispensing program executed in MAN, AUTO, and SEMI modes — Programs 1–4 — is selected via the PRGM knob on the CMDS panel. The PRGM knob has no effect in BYP or STBY.

Only Programs 1–4 are selectable. Programs 5 and 6 are independent of the PRGM knob position:

  • Program 5 is activated via the cockpit slap switch — outside the scope of CMS — and is not covered in this guide; see Dash-34 § 2.7.2.2 for details.
  • Program 6 is a special-purpose program always available for manual dispensing, independent of the PRGM knob position.

5.2.1.1 Manual Mode

In Manual (MAN) mode, the pilot executes countermeasure programs (1–4 and 6) via CMS Up and CMS Left.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
CMDS MAN Up Short Execute Program 1–4 Executes the program selected via the CMDS panel PRGM knob once per press. No threat sensing; no automatic triggering. Overrides any AUTO dispensing, if running. 2.7.2.2 18, 28
CMDS MAN Left Short Execute Program 6 Program 6 is dispensed independently of the PRGM knob position. 2.7.2.2 19

5.2.1.2 Automatic Mode

In Automatic (AUTO) mode, the ALE-47 CMDS dispenses the selected program (1–4) continuously in response to threats detected by the Radar Warning Receiver (RWR).

A CMS Down press grants consent for AUTO dispensing to start. It will continue until the pilot presses CMS Right or expendables are exhausted.

Even in AUTO mode, manual dispensing is still available.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
CMDS AUTO Up Short Execute Program 1–4 Executes the program selected via the CMDS panel PRGM knob once, interrupting any ongoing AUTO dispensing. After execution, AUTO resumes if the threat persists. 2.7.2.2 18, 28
CMDS AUTO Left Short Execute Program 6 Program 6 is dispensed independently of the PRGM knob position. Overrides AUTO; after execution, AUTO resumes. 2.7.2.2 19
CMDS AUTO Down Short Give Consent; Enable AUTO Dispensing Grants consent for AUTO dispensing. RWR-detected threats trigger automatic execution of the program (1–4) selected via the CMDS panel PRGM knob. Dispensing continues until the threat clears, the pilot presses CMS Right, or expendables are exhausted. Consent state persists if the pilot switches to MAN mode. If the pilot re-engages AUTO, dispensing resumes immediately on the next detected threat. 2.7.2.1 18, 28
CMDS AUTO Right Short Cancel Consent; Disable AUTO Removes CMDS consent and places the ALE-47 in Standby. Automatic dispensing halts immediately. The pilot must press CMS Down again to resume AUTO operation. 2.7.2.1 18, 28

5.2.1.3 Semi-Automatic Mode

In Semi-Automatic (SEMI) mode, the CMDS control unit displays DISPENSE RDY and sounds a COUNTER voice message every time a threat is detected. For each COUNTER voice message, a CMS Down press grants consent and the ALE-47 CMDS then dispenses one selected program.

Even in SEMI mode, manual dispensing is still available.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
CMDS SEMI Up Short Execute Program 1–4 Executes the program selected via the CMDS panel PRGM knob once, independent of RWR threat state. After execution, the CMDS returns to standby and resumes threat detection. 2.7.2.2 18, 28
CMDS SEMI Left Short Execute Program 6 Program 6 is dispensed independently of the PRGM knob position. After execution, the CMDS returns to standby and resumes threat detection. 2.7.2.2 19
CMDS SEMI Down Short Give Consent; Dispense One Program Dispenses one program (1–4) in response to a COUNTER voice message. Consent state is retained: if the pilot switches to AUTO, the CMDS begins dispensing immediately on the next detected threat. 2.7.2.1 18, 28
CMDS SEMI Right Short Cancel Consent; Return to Standby Removes SEMI consent and places the CMDS in Standby. COUNTER voice messages cease. 2.7.2.1 18, 28

5.2.1.4 Bypass and Standby Modes

In BYP and STBY, both non-combat modes, AUTO and SEMI dispensing are not available. Consent state is not tracked in either mode.

Bypass (BYP): In BYP, the CMDS program selection is bypassed: CMS Up dispenses exactly one chaff and one flare per press. Program 6 remains available via CMS Left.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
CMDS BYP Up Short Dispense One Chaff + One Flare The PRGM knob setting has no effect. AUTO and SEMI dispensing are not available in BYP. 2.7.2.1
CMDS BYP Left Short Execute Program 6 Program 6 is dispensed independently of the PRGM knob position. 2.7.2.2

Standby (STBY): In STBY, CMDS programs and bingo quantities can be edited via the UFC. This mode inhibits all chaff and flare release: no CMS direction produces a dispensing effect. For program editing procedures, see Dash-34 §§ 2.7.2.1 and 2.7.2.3.

5.2.2 ECM

The ECM system operates in two configurations:

  • External pods (ALQ-131, ALQ-184) — controlled via CMS Down; and
  • Internal IDIAS — controlled via CMS Left.

5.2.2.1 External ECM Pod (ALQ-131/ALQ-184)

For the external ECM pod to operate, its power switch must be in OPR. This enables the XMIT switch on the ECM control panel to set the operation mode:

  • XMIT 1: Avionics Priority, AFT antenna only
  • XMIT 2: ECM Priority, both FWD and AFT antennas
  • XMIT 3: Active Jam, continuous transmission

After setting the operation mode, CMS Down grants consent for ECM pod transmission. The ECM Enable light on the left miscellaneous panel illuminates.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
ECM Pod Down Short Grant ECM Consent The pod transmits in the operation mode set by the XMIT switch. Transmission continues until the pilot presses CMS Right or the RF switch is moved out of NORM. 2.7.4.1.1, 2.7.4.2.5 28
ECM Pod Right Short Remove ECM Consent ECM consent is removed. The pod is placed in Standby and the ECM Enable light extinguishes. The pilot must press CMS Down again to resume transmission. 2.7.4.1.1, 2.7.4.2.5 28

5.2.2.2 Internal ECM (IDIAS)

For IDIAS to operate, its power switch must be in ON. Then, with the XMTR switch in OPER, CMS Left cycles the ECM operation mode.

The active operation mode is displayed on the HUD, FCR, RWR, and TFR pages.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
IDIAS ECM Left Short Cycle ECM Operation Mode The IDIAS mode advances with each short press: STBYAVNC (Avionics Priority) → ECM (ECM Priority) → AVNCECM. 2.7.4.1.2 28
IDIAS ECM Right Short Set ECM to Standby IDIAS is set to STBY. The pilot must press CMS Left again to return to AVNC or ECM. 2.7.4.1.2 28

On aircraft equipped with an external ECM pod, CMS Down grants consent to both the ALE-47 CMDS and the external ECM pod. This joint consent applies to CMDS AUTO and SEMI modes only.

As CMS Down has no function on IDIAS-equipped aircraft, the joint consent does not apply.

Mode Dir. Act. Function Effect / Nuance Dash34 Train.
CMDS AUTO/SEMI + ECM Pod Down Short Joint Consent (CMDS + ECM) Simultaneous consent to CMDS and the external ECM pod. 2.7.2.1, 2.7.4.2.5 18, 28

5.2.4 Constraints and Edge Cases

State Tracking: In CMDS AUTO and SEMI modes, consent state is not cleared when MAN mode is selected. If the pilot re-engages AUTO or SEMI without pressing CMS Down, the CMDS begins dispensing immediately on the next detected threat. As BYP and STBY modes do not have a consent state, switching to either mode does not retain any prior consent.

Bingo Quantity Behavior: In AUTO mode, the CMDS continues dispensing when expendables fall to or below the bingo quantity. The pilot must press CMS Right to disable AUTO dispensing, or switch to MAN mode.

RF Switch Override: When ECM consent is active, the ECM system is placed in Standby if the RF switch is moved from NORM to QUIET or SILENT. Consent is not restored when the RF switch is returned to NORM. The pilot must press CMS Down again to resume ECM transmission.

Ground Safety: On the ground, if the pilot holds CMS Down, the ECM pod may radiate. Ground personnel must be clear of the radiation area.

5.3 Block and Variant Configurations

CMS interaction with CMDS is uniform across all F-16 block and variant configurations (see Section 5.2.1).

F-16 block and variant configurations with external pod ECM, however, use different CMS procedures and ECM control panels (see Section 5.2.2):

ECM Configuration CMS Direction Panel Control
External Pod (ALQ-131/ALQ-184) CMS Down (consent) XMIT switch (positions: 1, 2, 3)
Internal IDIAS CMS Left (mode cycling) XMTR switch (positions: STBY, OPER)

5.3.1 ECM Configurations by Block and Variant

The block and variant configurations listed in the following tables are sourced from Dash-34 documentation. Not all may be available as selectable aircraft in Falcon BMS 4.38.1.

5.3.1.1 ECM Pods (ALQ-131/ALQ-184)

These block and variant configurations use the ECM Pod Control Panel with manual jamming program selection. For detailed procedures, see Section 5.2.2.1.

Operator Block/Variant
USAF Blocks 40/42/50/52 (CM designation)
NATO Block 15 operators (Belgium, Denmark, Netherlands, Norway)
International Egypt, Korea KF-16C Block 32

5.3.1.2 Internal ECM (IDIAS)

These block and variant configurations use the IDIAS ECM control panel. For detailed procedures, see Section 5.2.2.2.

Operator Block/Variant
Israel F-16I Sufa Block 52, Barak I Block 30, Barak II Block 40
International Greek HAF (Blocks 50 PXII, 52 PXIII, 52+ PXIV Advanced), Korea KF-16C Block 52, Singapore F-16D Block 52