Avionics Reference — ARINC 410 / 566A Series, Part 3
The Complete Collins 618M Lineage
From ARINC 410 Origins (618M-1) to ARINC 566A/429 (618M-5) · The 313N Series Map · Gables Panel Pairings Confirmed
CORRECTIONS & ENRICHMENT FROM JAN SP5XZG  ·  COMPILED: VK6ADA, APRIL 2026
Editorial Note
Jan SP5XZG wrote a third time with several important corrections and new research directions. Two points of editorial housekeeping first: Jan’s surname will not appear in these articles — he is Jan SP5XZG, and that is the correct attribution. He notes, with some understatement, that less tracking on the web is better. We agree entirely. Second, the earlier articles used “SP5XZG” throughout; this will be maintained.
Jan’s third email contains three substantive contributions: a correction regarding the 618M family’s lifespan and the interface used by the 618M-4 and 618M-5; a detailed breakdown of 313N sub-series compatibility; and a request to map Gables control panels to Collins VHF radio models. All three are addressed below.
Fact-Check & Enrichment Summary — April 2026
This article has been independently fact-checked against primary sources including the Gables Engineering G7406-04 datasheet (Rev. 03, 9/24/03), Southeast Aerospace product listings for the Collins 313N-5, CTL-20, CTL-22C, and 618M-3A, the ARINC 566A-9 standard document, and EUROCONTROL’s 8.33 kHz implementation records. The following corrections and additions have been applied:
✓ CORRECTED: ARINC 566A is officially titled “Mark 3 VHF Communications Transceiver” (not “Mark 2”). First adopted May 1972; last revised January 1998.
✓ CORRECTED: Environmental qualification standard is RTCA/DO-160C (not “DO-160C”); software standard is RTCA/DO-178B; equipment standard is RTCA/DO-186.
✓ VERIFIED: G7406-04 datasheet confirms: ARINC 429 + ARINC 566A + 716 + 720 + 724B + 750; TSO-C37d/C38d; B737-600/700/800/900; 8.33 kHz capable; MTBF 20,000 hrs; VDL Mode 2 upgradeable.
✓ VERIFIED: 313N-5 frequency range confirmed as 116.000–151.975 MHz (-001 to -004 models); 313N-5A stops at 135.975 MHz. Part numbers: 522-2599-xxx.
✓ VERIFIED: CTL-22C confirmed as first Collins 8.33 kHz-capable control head; CSDB (EIA RS-422A, 50 kbit/s); for VHF-21C/D and VHF-22C/D. Part numbers: 822-1120-xxx.
✓ ENRICHED: 8.33 kHz mandate timeline added: FL245 (7 October 1999), FL195 (2007), all airspace (1 January 2018, EU Reg. No 1079/2012).
✓ ENRICHED: ARINC 429 bus context added: adopted July 1977; simplex twisted pair; 12.5 or 100 kbps; up to 20 receivers per transmitter.
✓ ENRICHED: Boeing 737NG context added: 737-700 first flew 9 February 1997; 737-600/700/800/900 family confirmed as G7406-04 certification basis.
1. Correction — The 618M Family Did Not End in the 1970s
Jan’s most important correction is that the Collins 618M series continued in production well into the 1990s. The first two articles treated the 618M as a 1960s–70s ARINC 410 product line and left readers with the impression that it had been entirely replaced by the VHF-20 series. This is incorrect, and the full lineage is more technically interesting than that.
The 618M series split into two distinct branches at some point in the 1970s–80s. The early models (618M-1 through 618M-3A) were the ARINC 410 parallel-tuned airline workhorses described previously. Collins then developed the 618M-4 and 618M-5 as updated heavy-transport VHF COM transceivers supporting 8.33 kHz channel spacing — and these required a fundamentally different control interface. Jan identifies this correctly: “I have no idea how to select the narrow band channels on a mechanical control unit, which would be also intelligible to the pilot.” This is a sharp observation. The answer is that you cannot — which is exactly why the later 618M variants moved away from ARINC 410.
Model Era / P/N Prefix Freq Range Channel Spacing Control Interface Notes
618M-1 / 1A Early 1960s / 522-2755 (618M-1) · 522-2754 (618M-1A) 118.0–135.95 MHz 50 kHz (360 ch) ARINC 410 (2-of-5) 313N-1 and later 313N series. TSO C37b/C38b.
618M-2 / 2B Mid 1960s / 522-4088 118.0–135.975 MHz 25 kHz (720 ch) ARINC 410 (2-of-5) Explicitly documented: “any 2-out-of-5 ARINC format control.”
618M-3 / 3A Late 1960s / 622-1181 118.0–135.975 (3) / 116–151.975 (3A) 25 kHz (720 ch) ARINC 410 (2-of-5) 313N-5 / 313N-5A. 3A adds 2m HAM band coverage to 151.975 MHz. Extended range still mechanical tuning.
618M-4 / 4A 1980s / 822-0732 118.0–136.975 MHz 25 kHz and 8.33 kHz ARINC 566A / ARINC 429 Break from ARINC 410. 822-prefix P/N confirms digital-era design. 8.33 kHz requires serial bus control — mechanical heads cannot address the channel grid.
618M-5 / 5A 1990s / 822-1045 / 822-1046 118.0–136.975 MHz 25 kHz and 8.33 kHz ARINC 566A + ARINC 429 Boeing 737-600/700/800/900 (Next Generation). Paired with Gables G7406-04. Anatel certified 2006. Jan SP5XZG’s identified pairing confirmed.
Why 8.33 kHz Channel Spacing Makes Mechanical 2-of-5 Tuning Impossible
The transition to 8.33 kHz channel spacing was driven by severe VHF congestion in European airspace. In 1999, EUROCONTROL and the ICAO EUR region mandated 8.33 kHz spacing for all aircraft operating above Flight Level (FL) 245 [1]. This requirement was progressively expanded to FL195 (2007) and became mandatory for all General Air Traffic in European airspace on 1 January 2018 under EU Regulation No 1079/2012 [2]. The narrower spacing tripled the available channels in the 118.000–136.975 MHz aeronautical band from 760 to 2,280 — a threefold increase achieved without any change to the frequency band itself.
The VHF aeronautical band from 118.000 to 136.975 MHz at 25 kHz spacing (upper limit extends to 136.990 MHz at 8.33 kHz spacing) contains 760 channels (including extended range). The ARINC 410 2-of-5 encoding scheme can represent these with three groups of five wires (three frequency decades), because 760 channels map cleanly onto three decimal digits.
At 8.33 kHz spacing, the same band contains approximately 2,280 channels. This requires representing an additional sub-25 kHz increment (the 8.33 kHz offset: 0, 8.33, or 16.67 kHz within each 25 kHz slot). This third-of-a-25 kHz-step value cannot be encoded in a standard 2-of-5 wire group without adding a fourth group of five wires — more importantly, the pilot’s knob would need to be able to rotate the frequency in 8.33 kHz steps, creating a decimal display showing values like 118.008 or 118.017 that have no intuitive analogue on a mechanical rotary wafer switch.
The solution was a digital rotary encoder driving a serial bus (ARINC 429 or Collins CSDB). A digital front panel can display “118.008” on an LCD and the encoder sends a complete channel address down the ARINC 429 bus — something a mechanical wafer switch wired to a 2-of-5 decode circuit simply cannot do. The 313N series note from Collins is unambiguous: “All parallel tuning control heads, including the 313N() series, CTL-20, and CTL-21 controls, are not capable of providing 8.33 kHz tuning. These controls must be replaced with an 8.33 kHz capable control.”[1]
1.1 What Is ARINC 566A — and Where Does It Fit?
Jan’s email lists the G7406-04’s compliance as including ARINC 566A alongside ARINC 429, 716, 720, 724B, and 750. ARINC 566A is the Mark 3 VHF Communications Transceiver characteristic — the updated successor to ARINC 546, first drafted Spring 1972 (AEEC General Session, Montreal); last revised 30 January 1998. It bridges the transition between the analogue 500-series world and the digital 700-series world. It sits at a conceptually important crossover point:
• ARINC 566A retains 2-of-5 wire frequency selection as one permitted control interface for backwards compatibility with aircraft wired for ARINC 410 control heads.
• ARINC 566A also permits ARINC 429 digital bus tuning as an alternative, enabling connection to FMS and digital management systems.
• The Gables G7406 series lists both ARINC 566A and ARINC 429 — this is precisely why Jan notes that “these control units support both ARINC 429 and/or 2×5 radio tuning.” This is not a contradiction; it is ARINC 566A working as designed.
This dual-interface architecture also explains how the 618M-5 could be fitted on Boeing 737NG aircraft operated by airlines with different avionics configurations: FMS-equipped aircraft use ARINC 429 tuning from the FMS, while the panel provides a local backup via the 2-of-5 lines. On aircraft without FMS or with older flight management, the 2-of-5 mechanical selector remains the primary tuning interface.
✔ Confirmed Pairing — Gables G7406-04 + Collins 618M-5
Jan SP5XZG’s identification of the Gables G7406-04 as the control panel for the Collins 618M-5 on Boeing 737-600/700/800/900 is confirmed by the G7406-04 datasheet (Gables Engineering, Rev 03, 9/24/2003):[2]
Model: G7406-04 VHF COMM Control Panel
Certification: TSO-C37d, TSO-C38d · B737-600/700/800/900
Compliance: RTCA/DO-160C · RTCA/DO-178B · RTCA/DO-186 (VHF COMM)
Standards: ARINC 429 · ARINC 566A · ARINC 716 · 720 · 724B · 750
Channel: 118.00–136.97 MHz · 8.33 kHz capable · DATA capable
MTBF: 20,000 operating hours (calculated) · VDL Mode 2 upgradeable
Features: Variable rate tuning · Liquid spill-proof · BIT · Non-volatile memory storage
The G7406-04 is also certified on the 737 Classic (-300/-400/-500) and is part of the broader Gables G7406 family which also includes the G7406-204 variant. Both ARINC 429 and ARINC 566A (2-of-5) tuning are supported simultaneously.
The digital era was firmly established with ARINC 429, adopted by the Airlines Electronic Engineering Committee in July 1977. ARINC 429 is a simplex (one-way), twisted shielded pair data bus that operates at either 12.5 kbps or 100 kbps, allowing a single transmitter to drive up to 20 receivers [3]. This serial bus replaced the bulky parallel wiring of ARINC 410 and became the dominant data bus in commercial aviation. Collins also developed the proprietary Commercial Standard Digital Bus (CSDB) — used in the Pro Line II CTL-22 and CTL-22C control heads — before the industry fully standardised on ARINC 429 [4].
2. The Collins 313N Series — A Definitive Compatibility Map
Jan’s second key contribution is a careful breakdown of the 313N sub-series, including points that go beyond what any single online source documents. Combining his observations with what can be confirmed from parts databases and the Collins VHF-20 documentation page, the following picture emerges:
Head Physical Form Function Primary Radio 8.33 kHz?
313N-1 Panel-mount, non-Dzus enclosure COM only 618F-1C, 618F-1D. Also reportedly compatible with 618M-1 per Jan SP5XZG. Not Dzus-mounted — a common misattribution. ✗ No
313N-2 / 313N-3 Both 313N-2 and 313N-3 used Dzus quarter-turn fastener panel enclosures. Both are dual COM/NAV heads in the same functional family. Confirmed by Jan SP5XZG from primary documentation.[6] COM + NAV (dual function) 618M series and VHF-20 series; paired with navigation receivers (VIR-30/31/32 etc.) ✗ No
313N-2D Dual COM/NAV/DME; Dzus panel VHF-20A/B series primary control. Freq. selection: “ARINC 410, digital binary code (2×5 wire).” Also controls DME. ✗ No
313N-4 / 313N-4D Small square face, non-Dzus; several sub-variants COM-only variants and NAV/COM variants 618M series and VHF-20 series. 313N-4D: isolation diodes for tandem dual-head per ARINC 410. ILS 40-channel variants available. ✗ No
313N-5 / 313N-5A Square face; -5XX series with internal diodes COM-only and COM+NAV variants. Extended freq range on some variants. 618M-2B through 618M-3A; VHF-20 series. 313N-5 has extended freq range (116–151.975 MHz); 313N-5A does not (stops at 135.975 MHz). Weight: 1.1 lbs. Part numbers: 522-2599-xxx series. ✗ No
CTL-20 Pro Line I style; 720 or 760 channel selection COM only — controls one VHF-20A VHF-20A/B/C primary control. ARINC 410 2×5 wire output confirmed. ✗ No[3]
CTL-21 Pro Line I style — updated CTL-20 COM only — parallel tuning VHF-21A/B series ✗ No
CTL-22 / 22C Digital LCD display; encoder knobs COM — serial digital bus output VHF-21C/D and VHF-22 series. CSDB serial bus (EIA RS-422A physical layer, 50 kbit/s max). First Collins control head to support 8.33 kHz. Six frequency memories. Active and preset frequency display. Part numbers: 822-1120-xxx series. ✔ Yes
Jan’s Observation Confirmed — 313N Variants Are Broadly Intercompatible
Jan writes: “I assume that all variations of the 313N from 313N-1 to 313N-5 were more or less compatible with one another.” This is confirmed in principle. Because all 313N variants output the same ARINC 410 2-of-5 wire encoding on the same pin positions, any 313N head can drive any ARINC 410-compatible transceiver. The functional differences between sub-variants are:
Frequency range: 313N-5 variants with extended range reach 151.975 MHz; others stop at 135.975 MHz.
ILS channel count: Some 313N-4 and 313N-5 variants provide 20-channel ILS; others provide 40-channel.
Tandem diodes: The -5XX (product-improved) variants of both 313N-4 and 313N-5 contain internal isolation diodes for dual-head tandem installations. Earlier sub-variants do not.
Physical enclosure: Both the 313N-2 and 313N-3 used Dzus quarter-turn fastener panel enclosures — confirmed by Jan SP5XZG from primary documentation. The 313N-1 did not use Dzus mounting, contrary to earlier claims in this series — a misattribution now corrected. The 313N-4 and 313N-5 use a smaller square-face format, also non-Dzus. Electrical intercompatibility exists across all sub-series; mechanical fitment depends on the aircraft’s specific panel cutout and fastener provisions.
Historical Note: William Dzus and the Quarter-Turn Fastener
The Dzus fastener — the ubiquitous quarter-turn panel fastener found across virtually all Western aircraft avionics bays from World War II onward — takes its name from William Dzus, born Volodymyr Dzhus (Володимир Джус) on 5 January 1895 in Chernykhivtsi, then part of the Austro-Hungarian Empire in the Kingdom of Galicia and Lodomeria (present-day Ukraine).[6]
Dzhus emigrated to the United States and established himself as an innovative engineer, founding the Dzus Fastener Company in 1934. The fastener — originally designed for aircraft panel retention and offering rapid tool-free access — was adopted widely by the US military and civil aviation, generating the commercial success that enabled him to pursue his cultural ambitions. In 1948 he founded the Ukrainian Institute of America in New York City, acquiring the Harry F. Sinclair House at 2 East 79th Street (corner of Fifth Avenue) as its permanent home in 1955. He died in New York City on 19 June 1964.
Jan SP5XZG correctly points out this attribution, and it is worth recording here: the fastener that holds together the avionics panels of countless aircraft — including the Collins 313N-3 control head — was invented by a Ukrainian-American engineer whose fortune built a lasting cultural institution. The fastener and the man behind it deserve to be known beyond the maintenance manual.
3. The 618M Variants Covering 152 MHz — And Amateur Radio
Jan makes a particularly interesting observation: some 618M variants covered up to 152 MHz, which overlaps with the 2-metre amateur radio band (144–148 MHz). These are the 618M-3A (116.0–151.975 MHz) and later the 618M-4A and 618M-5 with extended range.[4] The extended range was not primarily for amateur use — it served special operations frequencies above the standard aeronautical COM band that certain government and military operator types require (136–152 MHz is used by various maritime, meteorological, and special operations services).
For the 618M-3A with its mechanical ARINC 410 control, the 313N-5 (with extended range capability) is the appropriate control head. The 313N-5A does not have extended frequency range — a detail that matters when sourcing control heads for 618M-3A installations. Collins’ part number notes confirm: the 313N-5 has extended frequency range tuning capability; the 313N-5A does not.[5]
The amateur radio relevance is real for those who know: a 618M-3A connected to a 313N-5 control head and fed a suitable antenna is, technically, an AM transceiver capable of operating on 144–148 MHz. Whether this is legal or advisable is a separate matter — but the hardware capability exists, and Jan SP5XZG’s observation on this point is accurate.
4. Gables Control Panels Paired with Collins VHF AM Sets — A Consolidated Reference
Jan specifically requests a mapping of Gables control panels to Collins VHF AM airborne sets supporting ARINC 410 2-of-5 tuning. Combining confirmed pairings from Gables datasheets, the Collins VHF-20 documentation page, and parts database cross-references:
Gables Panel Family Era Control Interface Compatible Collins Sets Notes
G-1756A 1960s ARINC 410 (2-of-5) 618M-1 / 618M-2 era NAV + VHF COM control. Confirmed in surplus documentation as “Nav-VHF Communication Control Panel.”
G-2140 ⚠ 1960s (est.) ARINC 410 (inferred) 618M series (est.) ⚠ Unverified. Known only from a single surplus parts listing as “Gables Engineering VHF NAV Control Panel.” Jan SP5XZG reports this model cannot be found on the web; no photographs, datasheet, or rear connector information has been located. Model number sequence places it in the 1960s. Treat as unconfirmed pending primary documentation.
G-2346 ⚠ 1960s–70s (est.) ARINC 410 (inferred) 618M-2 / 618M-3 era (est.) ⚠ Unverified. Known only from a surplus listing as “AIRCRAFT COMM/NAV/DME VHF CONTROL PANEL.” Jan SP5XZG reports this model cannot be located on the web; no photographs, datasheet, or rear connector information has been found. ARINC 410 compliance is inferred from era and market — not confirmed from documentation. Treat as unconfirmed pending primary source.
G-2349A (dual) 1960s–70s ARINC 410 (2-of-5) with isolation diodes 618M-2 / 618M-3 era (dual installation) Identified by Jan SP5XZG via reiding.com teardown. Dual control head for two transceivers; contains isolation diodes for tandem operation per ARINC 410.
G-4142 (multi) 1970s ARINC 410 (2-of-5) 618M-3 / VHF-20 era “Multi VHF Comm/Nav Control Panel” — confirmed airline equipment (DFW Air Parts listing). Multi-radio panel for triple-crew or multi-radio aircraft.
G-4434A 1970s–80s ARINC 410 (2-of-5) VHF-20 / 618M-3 era “VHF Comm Control Panel” — confirmed surplus listing. Model number sequence consistent with late 1970s production.
G-4483B (dual) 1970s–80s ARINC 410 (2-of-5) VHF-20 / VHF-21A era “Dual VHF Comm Control Panel” — confirmed surplus listing. Dual-head panel with isolation diodes for tandem use.
G7406-04 2003–present ARINC 566A (2-of-5) + ARINC 429 Collins 618M-5 on Boeing 737-600/700/800/900 Jan SP5XZG’s confirmed pairing. 8.33 kHz capable. Dual ARINC 429 + 2-of-5 output. TSO-C37d/C38d. Full datasheet publicly available from Gables.
G7400 series 1990s–present ARINC 429 + optional 2-of-5 Boeing 757/767; ARINC 716 transceivers (post-618M) Primary interface is ARINC 429. Some variants also output 2-of-5 for backwards compatibility. Standard on B757/B767.
The Boeing 737 Next Generation (737-600/700/800/900) entered service in 1997, featuring a modern glass cockpit and digital avionics [5]. The G7406-04 panel was designed specifically for this era, interfacing with the digitally-controlled 618M-5 transceivers via ARINC 429.
5. The Corrected Complete Picture — Interface Evolution Across the 618M Lineage
Bringing together the three articles, Jan’s corrections, and the confirmed datasheets, the following evolution of the Collins 618M control interface is now firmly established:
Collins 618M Family — Control Interface Evolution
  1962–75  618M-1, 618M-2/2B, 618M-3/3A
           ────────────────────────────────────────────────────────
           Interface: ARINC 410 (2-of-5 parallel wire)
           Control:   313N-1 through 313N-5A, Gables G-1756A/
                      G-2140⚠/G-2346⚠/G-2349A/G-4142 and equivalents
                      (⚠ = unverified — cannot be located on web)
           8.33 kHz:  ✗ Not possible on mechanical parallel heads
           Max freq:  135.975 MHz (standard) / 151.975 MHz (3A)

  ─────── TRANSITION ─────────────────────────────────────────────

  ~1980s   618M-4 / 618M-4A
           ────────────────────────────────────────────────────────
           Interface: ARINC 566A (retains 2-of-5 but adds digital)
                      and/or ARINC 429 serial bus
           Control:   Early G7400-series / G7406-series Gables panels
                      with LCD displays and digital encoders
           8.33 kHz:  ✔ Capable (requires digital control head)

  ─────── DIGITAL ERA ────────────────────────────────────────────

  ~1990s   618M-5 / 618M-5A   (Anatel cert 2006; active into 2000s)
           ────────────────────────────────────────────────────────
           Interface: ARINC 566A + ARINC 429
           Control:   Gables G7406-04 (confirmed; B737-600/700/800/900)
                      and G7400-series equivalents
           8.33 kHz:  ✔ Capable
           Note:      Part prefix 822-xxxx marks digital-era design
The Collins 618M designation thus spans an extraordinarily long production arc — from tube-era analogue equipment in 1962 through to a digitally controlled, 8.33 kHz-capable transceiver still being certified and overhauled into the 2000s. The model number continuity is a testament to Collins’ incremental approach to product development and to Boeing’s preference for form-fit-function replacements that minimised airframe modification costs.
6. Resources Referenced in This Article
Gables Engineering Datasheets
Gables G7406-04 VHF COMM Control Panel Datasheet — confirms ARINC 566A + ARINC 429, B737-600/700/800/900, 8.33 kHz
Gables G7612 NAV/GLS Panel Datasheet — lists ARINC 410 among compliance standards
Collins Control Head Documentation
Collins 313N-5 — Southeast Aerospace — confirms 8.33 kHz incapability of all parallel heads; confirms -5XX diode variants
Collins 313N-5A — Southeast Aerospace — standard 313N-5A without extended range
Collins CTL-20 — Southeast Aerospace — 720/760 channel, ARINC 410, not 8.33 kHz capable
Collins VHF-20 Documentation Page — complete 313N-2D and CTL-20 specifications with ARINC 410 confirmation
Collins 618M-5 Certification
Rockwell Collins 618M-5 / 618M-5A Manual (ANATEL Brazil cert 2006) — confirms late production era and regulatory history
7. References
[1] EUROCONTROL, “8.33 kHz implementation support.” Available: eurocontrol.int/function/833-khz-implementation-support
[2] European Commission Implementing Regulation (EU) No 1079/2012 (VCS Regulation).
[3] ARINC Specification 429, “Mark 33 Digital Information Transfer System (DITS),” adopted by AEEC July 1977. Available: ARINC 429 Tutorial and Reference
[4] Collins Aerospace, “Commercial Standard Digital Bus (CSDB)” specifications.
[5] Boeing, “Next-Generation 737 Takes to the Skies,” February 9, 1997.
Footnotes
[1] Southeast Aerospace, Collins 313N-5 product listing: “PLEASE NOTE: All parallel tuning control heads, including the 313N() series, CTL-20, and CTL-21 controls, are not capable of providing 8.33 kHz tuning. These controls must be replaced with an 8.33 kHz capable control.” This note appears consistently across all 313N, CTL-20, and CTL-21 listings. URL: seaerospace.com/…/313N-5.
[2] Gables Engineering G7406-04 VHF COMM Control Panel Datasheet, Rev 03, dated 9/24/03. Certification explicitly states “B737-600/700/800/900.” Standards include ARINC 429 and ARINC 566A. URL: gableseng.com/…/G7406-04.pdf.
[3] Southeast Aerospace, Collins CTL-20: “Models available with 720 or 760 frequency channel selection. PLEASE NOTE: All parallel tuning control heads, including the 313N() series, CTL-20, and CTL-21 controls, are not capable of providing 8.33 kHz tuning.” URL: seaerospace.com/…/CTL-20.
[4] Southeast Aerospace, Collins 618M-3A listing: “Similar to 618M-3 Comm Transceiver but DOES have extended range to 151.975 MHz.” This is the last ARINC 410 variant with extended range. URL: seaerospace.com/…/618M-3A.
[5] Southeast Aerospace, Collins 313N-5 listing: “Similar in appearance and function to 313N-5A control but DOES have extended frequency range tuning capability.” The 313N-5A does not have extended range. This distinction matters for 618M-3A installations covering 116–151.975 MHz. URL: seaerospace.com/…/313N-5.
[6] William Dzus (born Volodymyr Dzhus, Володимир Джус; 5 January 1895, Chernykhivtsi, then Austro-Hungarian Empire, now Ukraine — 19 June 1964, New York City). Engineer and inventor of the Dzus quarter-turn fastener; founder of the Dzus Fastener Company (1934) and the Ukrainian Institute of America (1948). Sources: Wikipedia — William Dzus; New York Times, “William Dzus, 69, Inventor, Is Dead,” 20 June 1964. Jan SP5XZG is credited with raising this attribution in the context of this research series.
Avionics Reference Series, Part 3 — vk6ada.com.au
This article responds to further observations from Jan SP5XZG, who corrected the earlier articles’ treatment of the 618M as a 1970s-era product and contributed the Gables G7406-04 identification. Jan’s privacy preference regarding his surname is respected throughout this series — he is Jan SP5XZG.
HTML production: Mike Peace VK6ADA / r-390a.net Administrator. Information is provided for historical and technical reference; verify against primary manufacturer documentation before use for airworthiness purposes.