The King Radio KDM 7000B Distance Measuring Equipment

An illustrated, sourced deep dive into the "7000B DME": what it is, who made it, how airborne DME works, the related units, what is known about its insides, and how it was maintained. The author worked on the unit: he completed Bendix/King's "KDM 7000/A/B Digital DME Theory & Maintenance" course in January 1993, within his 1989–1996 period of radar and DME work.
By Rick Childers · September 2026

At a glance

The "7000B" is the King Radio KDM 7000B, an airborne DME interrogator: a radio box mounted in an airliner's electronics bay. It keeps asking a ground beacon "how far away am I?" and turns the beacon's answers into a distance readout in nautical miles for the pilots [1][2][5]. It is not a ground beacon. King Radio Corporation of Olathe, Kansas, built it; the company was part of Bendix/King under Allied-Signal by the late 1980s, and the product line is now Honeywell's [12][1][6][15]. Confirmed

Unit
KDM 7000B DME interrogator (transceiver); family KDM 7000, 7000A, 7000B, plus a "KDM 7000B (521D)" version [5][6][8]. Bendix/King's own 1993 course title groups them as "KDM 7000/A/B Digital DME" [29]
Role
Airborne, digital. King called the KDM 7000( ) a "digital ARINC 568 DME Interrogator" [2], and Bendix/King's 1993 course was titled "Digital DME Theory & Maintenance" [29]
Part numbers
066-1019-xx. CASA lists KDM 7000B dashes -21, -23, -26, -33, -43 and -57 [1]; a seller's data plate reads 066-1019-(2)7 [12]
Data plate
WT 18.3 lb; TSO C66a; DO-160 environmental category; 115 V ac 400 Hz 0.5 A; King Radio Corp, Olathe, Kansas [12] (read from a seller's photo)
Aircraft
Boeing 747 (Boeing maintenance manual) [4]; a unit sold from a retired Boeing 737 [12]
Related units
VHF NAV control/receiver (channeling), ARINC 568 indicators such as the King KDI 5710, King 499 synchro driver for ARINC 521D installations, L-band antenna, ASI-776-4 / Bendix/King 696-2795-00 test set [2][8][4]
Training
Bendix/King course "KDM 7000/A/B Digital DME Theory & Maintenance," Allied-Signal Aerospace Company, Jan. 18–22, 1993, completed by the author [29] Author's certificate
Safety action
Bendix/King Alert SB KDM 7000B-34-14 (Nov. 4, 1988) and FAA AD 88-25-01 (Dec. 20, 1988) on false NAV channeling [1][3]
DME basics
962–1213 MHz; 252 channels (126 X + 126 Y); pulse pairs 12 µs apart (X); ground reply delay 50 µs (X) or 56 µs (Y); measures slant range [17][19][20]
Not found
Transmitter power, receiver sensitivity, accuracy, dimensions and introduction date for the KDM 7000B itself Not found

How to read this page: each major section opens with a plain-language summary. Terms with a dotted underline link to the glossary, and hovering over one shows a short definition. Detailed tables and source discussion are in collapsible panels (▸), which expand automatically when printed. Colored tags show how well each statement is supported: Confirmed a source states it; Inferred reasoned from sources; Unverified a single weak source; Calculated arithmetic on cited values; Not found searched for and not found; Sources differ sources disagree.

1. What the "7000B" is

In briefThe name "Bendix/King 7000B DME" alone does not say whether it was an airborne unit or a ground beacon. The sources settle it: it is the KDM 7000B, an airborne DME interrogator built by King Radio Corporation in Olathe, Kansas, and sold under the Bendix/King name after King and Bendix were combined [1][12][15]. An Australian airworthiness directive from February 1989 names the "King KDM 7000B Distance Measuring Equipment" and its part numbers [1]. A Boeing 747 maintenance manual calls it a "KDM 7000/B DME interrogator" [4]. No ground DME called "7000" or "7000B" was found. The author's own training certificate from January 1993 names the family "KDM 7000/A/B Digital DME" [29].

DME, short for distance measuring equipment, is one of the oldest radio navigation aids still in daily use. A box in the aircraft (the interrogator) sends short radio pulses to a beacon on the ground (the transponder). The beacon answers after a fixed delay, and the aircraft works out the distance from how long the answer took to come back [17][18]. The pilots see a distance in nautical miles. So "DME" can mean either end of the link, which is why the question of airborne or ground had to be settled first.

Several independent sources tie the name to the airborne box. A repair station lists "066-1019-ALL Bendix/King KDM 7000A DME Transceiver" and "KDM 7000B DME" [5]. A test-set maker sells a "KDM-7000 Test Set" that tests the KDM-7000, 7000A and 7000B [8]. Honeywell's parts catalog still carries KDM 7000B maintenance and installation manuals and circuit cards [6]. A 1977 maintenance manual for a King accessory calls the KDM 7000( ) a "digital ARINC 568 DME Interrogator" [2]. ARINC 568 is the airline standard for the airborne Mark 3 DME [22]. Confirmed

Flight deck of a Boeing 737-200 (Canadian North, C-GDPA). One KDM 7000B on the market came from a retired 737 [12], so this is the kind of aircraft it served. This photo does not show a KDM 7000B, and the DME fitted to this particular aircraft is not known. The interrogator itself sat out of sight in the electronics bay; the crew saw only the distance readout and the NAV tuning controls.
Figure 1. Flight deck of a Boeing 737-200 (Canadian North, C-GDPA). One KDM 7000B on the market came from a retired 737 [12], so this is the kind of aircraft it served. This photo does not show a KDM 7000B, and the DME fitted to this particular aircraft is not known. The interrogator itself sat out of sight in the electronics bay; the crew saw only the distance readout and the NAV tuning controls.
Photo: Quintin Soloviev, 2024, via Wikimedia Commons [30], CC BY 4.0. Resized.
Firsthand evidence: training certificate (Rick Childers) Firsthand
The author completed a Bendix/King course in "KDM 7000/A/B Digital DME Theory & Maintenance" on January 18–22, 1993. The certificate names Bendix/King as presenter and Allied-Signal Aerospace Company as the parent, and carries form number 058-02638-0001 [29]. It is primary evidence for three points: Bendix/King itself described the unit as a digital DME; it trained technicians on the KDM 7000, 7000A and 7000B together as one family; and in January 1993 Bendix/King was part of Allied-Signal Aerospace. His radar and DME work as a whole spanned 1989 to 1996. The scanned certificate is on a companion page (link below).

1.1 Candidates considered

Three possibilities were considered. Each was checked against sources rather than assumed.

CandidateWhat the sources sayVerdict
King KDM 7000B airborne DME interrogatorNamed in CASA AD/RAD/45 with P/Ns 066-1019-xx [1]; "KDM 7000B" on the King Radio data plate in a seller's photo [12]; KDM 7000/B interrogator in the Boeing 747 AMM [4]; KDM 7000B in repair and test-equipment catalogs [5][8]Confirmed This is the "7000B"
Bendix DMA-37AA different DME interrogator, P/N 2041167 series, from the Bendix air-transport line; listed on 737, 747, 757, 767 and A320 [28]. No source calls it a "7000B."Rejected: different unit
Ground "DME 7000" beaconFAA Order 6820.14 lists the ground DMEs in FAA service: Cardion FA-9639 and FA-9783, ASII 1118, Selex FA-30600/30601, Thales FA-18200 and 415SE, and Wilcox FA-9996 and FA-10391 [17]. None is a "7000" and none is a Bendix/King product.Rejected: no such beacon found Not found
A "DME-7000" series from Bendix's air-transport divisionNot found. The "7000" number belongs to King Radio's KDM (King DME) model series, like the earlier KDM 700 [27].Rejected Not found
Why "Bendix/King" and not just "King"?company names on the documents

The data plate on the seller's unit reads "KING RADIO CORP, OLATHE, KANSAS 66061 USA" [12]. The 1988 service bulletin was issued as a "Bendix/King Alert Service Bulletin" [1], and the FAA filed AD 88-25-01 under "Bendix/King" [3]. That matches the corporate history: Allied Corporation bought King Radio and Bendix, and the combined avionics business traded as Bendix/King [15][14]. Today the manuals and parts are catalogued by Honeywell Bendix King [6]. The name "Bendix/King 7000B DME" is therefore the right one for the late-1980s and 1990s period, and the author's 1993 certificate shows Bendix/King presenting its own KDM 7000/A/B course under the Allied-Signal Aerospace Company name [29].

The KDM 7000B came from King's Olathe side of the business. The RDR-4A weather radar, the subject of an earlier document in this series, came from Bendix's air-transport avionics division in Fort Lauderdale. Both carried the Bendix/King name under Allied-Signal in 1989–1996.

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2. History: King Radio, Bendix/King, Allied-Signal, Honeywell

In briefEd King founded King Radio in 1959 and soon moved it to Olathe, Kansas [15][14]. The company was best known for light-aircraft radios but also built airline equipment, starting with the all-solid-state KTR 900 transceiver in 1966 [14]. The KDM 7000 existed by February 1977, when a maintenance manual for a King accessory named it [2]. Allied bought Bendix in 1983 and King Radio in 1983 or 1985 (sources differ), and the two were merged as Bendix/King [15][14]. In late 1988 a service bulletin and an FAA airworthiness directive required a fix to certain KDM 7000B units [1][3]. The line passed to Honeywell with the 1999 merger [16].

King Radio, Bendix/King and the KDM 7000 family: timeline (original diagram)196019701980199020002010202020301959: King Radio founded (Olathe, Kansas)1966: KTR 900 solid-state airline transceiverby Feb 1977: KDM 7000( ) exists (499 synchro driver CMM)Nov–Dec 1988: SB KDM 7000B-34-14; FAA AD 88-25-011983: Allied acquires Bendix; King acquired 1983 or 19851985: Allied-Signal formed1989–1996: author's radar/DME work; Jan 1993 KDM 7000/A/B course1999: AlliedSignal merges with Honeywell2026: manuals still in Honeywell catalog
Figure 2. Company and product timeline, drawn for this document from the cited sources. The shaded bar is 1989–1996, the author's period of radar and DME work; he completed the Bendix/King KDM 7000/A/B course in January 1993 [29].
Dated events tablewith sources
DateEventSource
1959Ed King founds King Radio Corporation near Kansas City; it soon moves to Olathe, Kansas[15][14]
1966King produces the KTR 900, an all-solid-state airline transceiver[14]
1966–1972King Radio files a series of DME patents: digital distance measuring, rapid search, DME indicator, search/track decision circuit[26]
by Feb. 1977The CMM for the King 499 synchro driver describes use with the "King Radio Model KDM 7000( ) digital ARINC 568 DME Interrogator"[2]
1981–1986King Radio patents a microprocessor DME that correlates replies over several interrogations (US 4,599,617; application first filed June 1981)[25]
1983Allied Corporation acquires Bendix. Wikipedia says Allied also acquired King Radio in 1983 and formed Bendix/King; the same article and Flying Tin also place the King sale in 1985 Sources differ[15][14]
Late 1985Allied merges with The Signal Companies to form Allied-Signal[16][14]
Nov. 4, 1988Bendix/King Alert Service Bulletin KDM 7000B-34-14 issued[1]
Dec. 20, 1988FAA AD 88-25-01, "Bendix/King Distance Measuring Equipment"[3]
Feb. 1989Australia issues AD/RAD/45 (compliance within 150 h time in service after Feb. 23, 1989, or before May 23, 1989, whichever is sooner)[1]
Jan. 18–22, 1993Bendix/King presents its "KDM 7000/A/B Digital DME Theory & Maintenance" course; the certificate is printed "Allied-Signal Aerospace Company"; the author completes it Author's certificate[29]
1993Allied-Signal renamed AlliedSignal[16][14]
1999AlliedSignal merges with Honeywell and takes the Honeywell name[16]
2026KDM 7000/7000A/7000B manuals and cards still listed in the Honeywell Bendix King catalog; units still sold on the surplus market[6][12]

The introduction date of the KDM 7000 is not documented in anything found Not found. The 1977 CMM date is only the latest possible date for the basic model, and the letter suffixes (A, B) came later. The dates of the 7000A and 7000B are also unknown. The 1988 service bulletin is numbered -34-14, and a -34-12 also exists [1][7], If those numbers run in sequence, the 7000B had already collected a dozen or more bulletins by late 1988, which would suggest a unit several years into service. The numbering scheme is not confirmed, so treat this as a hint only. Inferred

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3. The units and how they connect

In briefA KDM 7000B installation is more than one box. The pilots tune the DME from the VHF NAV control panel: selecting a VOR or ILS frequency also selects the paired DME channel, and the DME and NAV receiver share the same channel-selection wires [1][22]. The KDM 7000B sits in the electronics bay, runs on 115 V ac 400 Hz aircraft power [12], and sends distance to the cockpit indicators as ARINC 568 digital data [2][22]. It talks to the ground through an L-band antenna on the underside of the fuselage [22][31]. Older aircraft wired for analog DME used a King 499 synchro driver to convert its output [2].

KDM 7000B DME installation: units and connections (original diagram)FLIGHT DECKELECTRONICS (EE) BAYFUSELAGE / OTHER SYSTEMSVHF NAV control panelpilot selects VOR/ILS frequency(DME is tuned with it)DME indicator(s)ARINC 568 digital type,e.g. King KDI 5710 (use incockpit not confirmed)Older analog (ARINC 521D)indicators / RMI distancevia King 499 synchro driverKDM 7000BDME interrogator(transceiver)P/N 066-1019-xx115 V ac 400 Hz, 0.5 A18.3 lb, TSO-C66arear connectors P7001/P7002King 499 synchro driver(PED CMM 34-50-01)Aircraft 115 V ac 400 Hz busVHF NAV receivere.g. King KNR 6030 orCollins 51RV-4 (747 AMM)L-band DME antennablade, fuselage underside(part number not found)Other L-band systemsATC transponder, TCAS(suppression line, ARINC 568)Shop only: top test connectorused with ASI-776-4 / 696-2795-00channeling(2-of-5 code)same channeling lines, paralleled (see AD 88-25-01)ARINC 568distance data568 dataanalogcoaxTX/RXsuppressionSolid boxes: confirmed by sources. Dashed orange: inferred from the ARINC 568 standard, not confirmed for this installation. Grey: related equipment.
Figure 3. KDM 7000B system interconnect, drawn for this document. The NAV receiver examples (King KNR 6030, Collins 51RV-4) come from the Boeing 747 AMM [4]; the 499 synchro driver from its CMM listing [2]; the rear connector names from a seller's photos [12]. Items drawn dashed are what the ARINC 568 standard provides for [22], not confirmed for any particular KDM 7000B installation.
UnitWhat it doesPart number / modelSource
KDM 7000B DME interrogatorTransmits interrogations, receives replies, computes distance, outputs ARINC 568 data066-1019-xx (see §6)[1][12]
VHF NAV control panelPilot selects a VOR/ILS frequency; the paired DME channel is selected on the same wires. ARINC 568 specifies a "two-out-of-five" binary frequency-selector code and a common VHF NAV/DME selectorModel not identified Not found[22][1]
VHF NAV receiverShares the channeling lines with the DME. The 747 AMM names the Collins 51RV-4 and King Radio KNR 6030KNR 6030; Collins 51RV-4[4]
DME indicator(s)Shows distance. ARINC 568 defines a "standard distance indicator" fed with serial BCD and 26 V ac, in electromechanical and light-bar typesKing KDI 5710 and KDI 5700 manuals exist; the KDI 5710 is required on the bench for the ASI-776-4. Cockpit use and unit P/Ns not confirmed Inferred[22][6][8]
King 499 synchro driverLets the digital ARINC 568 interrogator work in an aircraft wired for an analog ARINC 521D DMEKing P/N 068-1013; CMM 34-50-01 by Pacific Electro Dynamics (Feb. 1977)[2]
DME antennaL-band antenna, flush or blade type per ARINC 568, on the fuselage undersideP/N not found Not found[22][31]
Other L-band equipmentARINC 568 provides a suppression-pulse line so the DME and other L-band transmitters (e.g. ATC transponder) do not jam each otherNot confirmed for KDM 7000B Inferred[22]
Shop test setBench test of KDM 7000/7000A/7000BBendix/King 696-2795-00; ASI-776-4 equivalent[8]
Where the antennas are on a typical jet airliner. Item 5 in the drawing's legend is the DME antenna, a small blade on the underside of the fuselage (it appears in both the top and bottom views). The legend on the Commons page labels DME "S/R SHF"; DME actually works at about 1 GHz, in the L band (UHF). This is a generic drawing, not a KDM 7000B installation.
Figure 4. Where the antennas are on a typical jet airliner. Item 5 in the drawing's legend is the DME antenna, a small blade on the underside of the fuselage (it appears in both the top and bottom views). The legend on the Commons page labels DME "S/R SHF"; DME actually works at about 1 GHz, in the L band (UHF). This is a generic drawing, not a KDM 7000B installation.
Drawing: Tosaka, 2010, via Wikimedia Commons [31], CC BY-SA 3.0. Unmodified.
The ARINC 568 connection in more detaildata bus, outputs, power

ARINC 568 is the airline "characteristic" for the Mark 3 airborne DME. It sets the box's form factor, connectors and pin coding, the wiring between units, and the signals, so that one airline's DME can be swapped for another maker's [22]. Its table of contents shows what an ARINC 568 installation provides:

  • Outputs: serial BCD distance, analog distance, a range-rate pulse, distance-trip data and an aural (ident) output [22].
  • Range features: 200 NM search-range limiting with an override switch, ILS-DME provisions and a "memory" mode that holds the last distance briefly when replies drop out [22].
  • Power: primary power input, a 26 V ac output for the indicators, and power-control circuitry [22].
  • Control panel: common VHF NAV and DME frequency selectors, off-on and on-standby controls, and the two-out-of-five binary code for frequency selection [22].
  • Other: suppression pulses, echo susceptibility, functional test, indicator status monitoring and provisions for automatic test equipment [22].

The ARINC 568 data bus is a six-wire link: three differential pairs carrying clock, word sync and data, at about 11 kHz and 12 V nominal. Each word is 32 bits, an 8-bit label followed by 24 data bits [23]. It is an older, different bus from the ARINC 429 used on later airliners.

Which of these optional outputs a given KDM 7000B provided is not documented in anything found. The existence of a separate "KDM 7000B (521D)" maintenance manual and installation manual [6], and of ARINC 568 Appendix 5 "Adapting ARINC 521D installations to accommodate ARINC 568 units" [22], suggests a version configured for aircraft originally wired for the older ARINC 521D analog DME. Inferred

Rear connectors and data plate (from a seller's photos)read from listing photos, not reproduced

The Whaletail Sales listing photos [12] show a black-finished box with a front label "KDM 7000B DME, SERIAL NO., MODS, KING 066-1019-". The rear carries two connectors marked P7001 and P7002 and a connector marked "TOP CONNECTOR – FOR SHOP USE ONLY." The data plate reads, as far as can be made out:

KDM 7000B DISTANCE MEASURING EQUIPMENT · P/N 066-1019-[27, partly masked] · SERIAL NO. [masked] · WT 18.3LBS · TSO C66a · DO160 ENV CAT A2D2/A0XXXXXXAAAAZ · 115VAC 400Hz 0.5a · KING RADIO CORP, OLATHE, KANSAS 66061 USA

The environmental-category string is hard to read in the photo and should be treated as approximate. The seller's text gives the part number as "006-1019-27," which is almost certainly a typing slip for 066-1019-27 (King's unit numbers begin 066-; 006- is King's manual prefix) Inferred. The photos are the seller's property and are linked in §12, not reproduced.

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4. How DME works

In briefDME measures distance by timing a radio echo that is answered, not reflected. The aircraft sends a pair of pulses; the ground station hears them, waits exactly 50 µs (on reply delay (50 or 56 µs).">X channels) and sends a pair back on a frequency 63 MHz away. The aircraft measures the total time, subtracts the 50 µs, and divides by about 12.36 µs for each nautical mile of distance there and back [17][19][20]. The result is the straight-line slant range to the station, not the distance over the ground [18].

4.1 Two-way ranging

FAA Order 6820.14 describes it this way: when the pilot or flight management computer selects a ground station, "the airborne interrogator sends out distance interrogation pulses on the receiving channel frequency assigned to the ground station." The ground station receives them, delays them "a fix[ed] amount," and transmits replies back on the assigned channel. Because radio travels at a known speed, the elapsed time gives the distance. "Timing circuits on the aircraft measure the time intervals between the interrogation and reply, subtract the 50 or 56 µs delay, and convert the remaining time difference to distance," which is then displayed or sent digitally to other equipment [17]. Confirmed

"DME Two-way Ranging Concept." The interrogator (aircraft) sends a pulse pair; the ground transponder waits a fixed reply delay (50 µs on X channels, 56 µs on Y) and answers with its own pulse pair; the interrogator measures the total elapsed time.
Figure 5. "DME Two-way Ranging Concept." The interrogator (aircraft) sends a pulse pair; the ground transponder waits a fixed reply delay (50 µs on X channels, 56 µs on Y) and answers with its own pulse pair; the interrogator measures the total elapsed time.
Source: FAA Order 6820.14, Siting Criteria for Distance Measuring Equipment, 2023, Figure 2-2 [17]. U.S. Government work, public domain. Cropped from the rendered page.
One DME measurement, X channel (original diagram, not to scale)Aircraft (interrogator)Ground station (transponder)12 µstravels at the speed of lightfixed reply delay: 50 µs (X) or 56 µs (Y)12 µselapsed time T measured by the interrogatordistance (NM) = (T − reply delay) ÷ 12.36 µs; example: T = 173.6 µs on X → (173.6 − 50) ÷ 12.36 ≈ 10 NMSchematic: delays are timed between corresponding pulses; exact reference points are defined in the standards. Figures from FAA Order 6820.14, Wikipedia and airnav.eu (see text).
Figure 6. The same measurement drawn as a timeline, with a worked example: a reply arriving 173.6 µs after the interrogation on an X channel means (173.6 − 50) ÷ 12.36 ≈ 10 NM Calculated. The 12.36 µs per nautical mile round trip is from Wikipedia and airnav.eu [19][20].

4.2 Pulse pairs, X and Y channels

DME never sends single pulses. Each interrogation and each reply is a pair of pulses a fixed time apart, and the spacing tells the receiver whether the pair is meant for it. Each pulse is about 3.5 µs wide [20]. There are two families of channels [17][19][20]:

X channelsY channelsSource
Interrogation pulse spacing12 µs36 µs[17][20]
Reply pulse spacing12 µs30 µs[19][20]
Ground reply delay50 µs56 µs[17][20]
Number of channels126 (1X–126X)126 (1Y–126Y)[17]
VHF frequency pairingNAV frequencies ending in .x0NAV frequencies ending in .x5 (50 kHz steps)[20]

X channels came first; Y channels were added later for more capacity [19]. Whether the KDM 7000B covered Y channels as well as X channels was not found in any source Not found.

4.3 The frequency plan and VOR/ILS pairing

DME uses the band from 960 to 1215 MHz [17][18]; the 252 assigned frequencies run from 962 to 1213 MHz in 1 MHz steps [19]. Aircraft always interrogate between 1025 and 1150 MHz. The ground station replies 63 MHz above or below the interrogation frequency, and which way depends on the channel [19][20][21]. Frequencies around 1030 and 1090 MHz are kept free because the air traffic control radar beacon system (SSR) uses them [19][21].

DME channel plan, 962–1213 MHz (original diagram)Air-to-ground(interrogations)channels 1–126, X and Y: 1025–1150 MHzGround repliesX channels1X–63X: 962–102464X–126X: 1151–1213Ground repliesY channels64Y–126Y: 1025–10871Y–63Y: 1088–11501030 SSR1090 SSR98010001020104010601080110011201140116011801200MHzEvery reply is 63 MHz above or below its interrogation. X: 12 µs pulse spacing both ways, 50 µs delay. Y: 36 µs interrogation, 30 µs reply, 56 µs delay.Red lines: secondary-surveillance-radar frequencies kept clear of DME assignments. Sources: Wikipedia, airnav.eu, NRAO EDIR 313, FAA Order 6820.14.
Figure 7. DME channel plan drawn for this document from Wikipedia, airnav.eu and NRAO EDIR 313 [19][20][21]. X-channel replies fall at the two ends of the band; Y-channel replies fall inside the interrogation band.

Pilots never select a DME channel number directly. Each DME channel is paired with a VHF VOR or ILS frequency, and tuning the VHF NAV frequency tunes the DME too [19][20]. Channels 17 to 56 pair with 108–112 MHz (odd tenths for ILS, even tenths for VOR) and channels 57–59 and 70–126 with VOR frequencies from 112 to 117.95 MHz; channels 1–16 and 60–69 are not paired with VHF NAV frequencies [20]. This pairing is why the KDM 7000B shares channel-selection wires with the NAV receiver, and why a fault in one could mis-tune the other (§8.4) [1][4].

Channel arithmetichow an interrogation frequency maps to a reply

Interrogation frequencies for channels 1 to 126 run from 1025 to 1150 MHz, the same for X and Y [19]. The reply rule, as given by airnav.eu [20]:

ModeInterrogation 1025–1087 MHzInterrogation 1088–1150 MHz
Xreply = interrogation − 63 MHz (962–1024)reply = interrogation + 63 MHz (1151–1213)
Yreply = interrogation + 63 MHz (1088–1150)reply = interrogation − 63 MHz (1025–1087)

Example from the same source: a Y-mode ground station replying on 1042 MHz is channel 81Y, and the aircraft interrogates on 1042 + 63 = 1105 MHz [20].

4.4 Search, track, squitter and identification

Many aircraft use one ground station at once, and every aircraft hears every reply. To pick out its own replies, each interrogator sends its pulse pairs at deliberately irregular ("jittered") intervals. Only the replies to its own interrogations come back at a steady delay; replies meant for other aircraft arrive at random times [25][20]. In search mode the interrogator sends about 150 pulse pairs per second and looks for a delay that repeats. Once it finds one it locks on and drops to track mode at no more than about 30 pairs per second [19][20][21]. A King Radio patent notes that older designs took "from one to two seconds" to lock on [25].

The ground station also transmits squitter, pulse pairs not triggered by any interrogation, which keep its output steady and are ignored by aircraft because they are not synchronous with their interrogations [17][20]. About every 30 seconds the station keys its Morse identifier [17]. The DME ident tone is 1350 Hz, against 1020 Hz for the VOR or localizer, and is heard about once for every three or four VOR idents [18][19]. The station gives priority to the ident, then to distance replies, then to squitter [17]. A typical ground transponder can answer about 2,700 pulse pairs per second, enough for roughly 100 aircraft; beyond that it reduces receiver sensitivity so the most distant aircraft are dropped first [19][20].

4.5 Slant range, range and accuracy

DME measures the straight line from the aircraft to the station, which the AIM calls slant range. The AIM notes that the difference between slant range and ground distance "increases with aircraft altitude and proximity to the NAVAID" [18]. Far from the station the two are nearly the same; directly overhead, the DME reads roughly the aircraft's height above the station. Inferred

Slant range versus ground distance (original diagram)DME ground stationslant range (what DME measures)altitudeground distanceExample (calculated): 6 NM up, 8 NM out → DME reads √(6² + 8²) = 10 NM.Directly over the station at 6 NM (about 36,000 ft) it still reads about 6 NM.The error is small far from the station and large close in and high up. Source for the concept: AIM 1-1-7, FAA Order 6820.14.
Figure 8. Slant range geometry, drawn for this document. The worked numbers are simple Pythagoras on assumed values Calculated; the concept is from the AIM [18].

The AIM says reliable DME signals may be received out to 199 NM at line-of-sight altitude, with accuracy "better than 1/2 mile or 3 percent of the distance, whichever is greater" [18]. ICAO recommends an error no larger than 0.25 NM plus 1.25% of the distance [19][20]. FAA ground facilities are classed by standard service volume: Terminal (out to 25 NM, up to 12,000 ft), Low (40 NM, up to 18,000 ft) and High (up to 130 NM between 18,000 and 45,000 ft), plus newer DME Low and DME High volumes [18]. The ARINC 568 standard for the airliner's box adds 200 NM search-range limiting [22]. The KDM 7000B's own accuracy figure was not found Not found.

4.6 The ground end

The KDM 7000B is only half of the system. The ground station consists of a transponder, antenna, monitor and control unit. The monitor checks reply delay, reply efficiency, pulse spacing, pulse count, identification, radiated power, receiver sensitivity and transmitter frequencies. If a parameter goes out of limits, a single-transponder station shuts down and a dual station transfers to its standby equipment [17]. A typical en-route or terminal ground transponder has a 1 kW peak output [19]. DMEs are commonly co-located with a VOR (VOR/DME), an ILS (ILS/DME) or a TACAN (VORTAC) and share its identifier [19][20][18].

The VOR/DME ground station at Ronald Reagan Washington National Airport (DCA). The large ring of antennas is the VOR. This is the kind of station a KDM 7000B-equipped airliner interrogated. It is not associated with any particular airborne unit.
Figure 9. The VOR/DME ground station at Ronald Reagan Washington National Airport (DCA). The large ring of antennas is the VOR. This is the kind of station a KDM 7000B-equipped airliner interrogated. It is not associated with any particular airborne unit.
Photo: MediaGuy768, 2023, via Wikimedia Commons [32], CC BY-SA 4.0. Unmodified.

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5. Inside the KDM 7000B

In briefNo schematic, block diagram or internal photo of the KDM 7000B was found in public sources. What does survive is a list of its replaceable assemblies in Honeywell's parts catalog: numbered circuit cards (1, 3, 4 and 6 are listed), a VCO, buffer, divider-mixer, preselector, duplexer and IF board [6], plus a tuning mechanism sold by a parts dealer [13]. Those names outline a conventional DME transceiver, but the functions assigned to each card below are reasoned from the names, not from a King document. A 1980s King Radio patent shows how the company's engineers approached microprocessor DME design, but it is not confirmed to describe the KDM 7000B.

KDM 7000B assemblies named in the Honeywell catalog (original diagram, arrangement schematic)Boxes show catalog names only. Physical layout, card functions and signal flow are NOT from a source; grey boxes are gaps.RF / IF assemblies (KDM7000/A/B)Duplexer200-00133-0000Preselector200-00132-0000Divider mixer200-00135-0001VCO200-00126-0000Buffer200-00127-0000IF board200-00178-0000Numbered cardsCard 1 "FRQ"200-00120-0000 (7000B)Card 2not foundCard 3200-00122-0010 (7000B)Card 4200-00123-0000/-0001Card 5not foundCard 6200-00125-0003 (A/B)Tuning mechanism076-00340-0001 "TUNING MEC KDM7000" (parts seller)Power supply, processor, front-panel testno catalog names foundRear panel (from a seller photo)P7001 and P7002 connectors;"TOP CONNECTOR – FOR SHOP USE ONLY" test connectorSources: Honeywell Bendix King product reference catalog via Aeroval, pp. 1025–1026; Aircraft Parts Store; Whaletail Sales listing photos.
Figure 10. KDM 7000B assemblies named in the Honeywell Bendix King catalog [6] and by a parts seller [13], drawn for this document. The arrangement is schematic. Cards 2 and 5 were not found under KDM 7000 names Not found.

5.1 Cards and modules

Catalog P/NCatalog descriptionApplies toLikely role (inferred from the name)Source
200-00120-0000KDM7000B CARD1 FRQ7000B"FRQ": frequency / channel-selection logic Inferred[6]
200-00122-0000KDM7000/A CD #37000, 7000ACard 3 (function not stated)[6]
200-00122-0010KDM 7000B CARD #37000BCard 3, 7000B version (function not stated)[6]
200-00123-0000 / -0001KDM7000/A/B CARD 4allCard 4 (function not stated)[6]
200-00125-0003KDM7000/A/B CD 6 SallCard 6 (function not stated)[6]
200-00125-0023KDM7000 CARD #67000Card 6, basic 7000 version[6]
200-00126-0000KDM7000/A/B VCOallVoltage-controlled oscillator: generates the tunable RF for the selected channel Inferred[6]
200-00127-0000KDM7000/A/B BUFFERallBuffer amplifier after the oscillator Inferred[6]
200-00135-0001DIVIDER MIXER 70007000 familyFrequency divider / mixer, probably for the synthesizer loop or receiver conversion Inferred[6]
200-00132-0000KDM7000/A/B PRESLTallPreselector: tuned filter ahead of the receiver Inferred[6]
200-00133-0000KDM7000/A/B DUPLXRallDuplexer: lets the transmitter and receiver share one antenna Inferred[6]
200-00178-0000KDM7000/A/B IF BDallIntermediate-frequency amplifier and pulse detection Inferred[6]
076-00340-0001TUNING MEC KDM70007000 familyTuning mechanism assembly, possibly for mechanically tuned RF stages Inferred[13]
not foundCard 2, card 5, transmitter, power supply, processor/range computer—Gaps Not found—

Several of these assemblies are shared across the KDM 7000, 7000A and 7000B ("KDM7000/A/B"), while cards 1 and 3 have separate 7000B part numbers [6]. That suggests the three models share an RF section and differ mainly in the digital cards. Inferred The catalog descriptions are abbreviated and may not reflect how King's maintenance manual names the assemblies. The KDM 7000B maintenance manual (006-05155-0005) and the "KDM 7000B (521D)" manual (006-05164-0001) would settle these questions [6].

A plausible signal path, and why it is only plausiblereasoned from the part names and DME principles

Every airborne DME has to do the same jobs: generate a pulse-modulated transmitter signal on one of 126 interrogation frequencies; pass it through a duplexer to the antenna; receive the reply 63 MHz away; convert it to an intermediate frequency; detect pulse pairs with the right spacing; and time them against its own interrogations [17][19]. The KDM 7000B part names fit that pattern: VCO and buffer (signal source), divider-mixer (frequency control or conversion), duplexer (shared antenna), preselector (receiver front-end filtering), IF board (amplification and detection), and a "FRQ" card for channel selection [6]. Inferred

What cannot be said without the manual: whether the transmitter used vacuum-tube cavities or transistors, what the local-oscillator scheme was, which card holds the range-measuring logic, and whether the unit used a microprocessor. The presence of a "tuning mechanism" hints at a mechanically tuned element, but no source explains it. Not found

5.2 King Radio's DME design thinking (patent evidence)

King Radio held a series of DME patents. In 1966–1970 it filed for a digital distance-measuring method, a rapid-search technique, a DME indicator and a search/track decision circuit [26]. In 1981 King engineer James L. Stolpman filed for a microprocessor-based DME, granted in 1986 as US 4,599,617 [25].

The patent describes the problem any DME faces: the aircraft hears the replies to every aircraft using the station, so it must sort out which replies are its own. Older designs checked one reply per interrogation against a fixed-width range gate and took "from one to two seconds" to lock on. King's method stored every reply received after each interrogation. After a new channel was tuned, the unit made three interrogations before analyzing anything. It then compared each range figure from the latest interrogation with those from the previous seven, using a range gate whose width varied with the time between interrogations and with whether the unit was already locked. Statistical tests guarded against locking onto noise or squitter [25]. The circuit shown includes a microprocessor, a range counter and latch, RAM, a pair of shift registers for self-test, and an analog pulse-pair output for other equipment [25].

Sheet 1 of King Radio's US 4,599,617. Fig. 1 is the basic block diagram: clock, counter, latch, RAM and microprocessor (MPU), with decoded video from the receiver setting a flip-flop to capture each range count. Fig. 2 shows how the range gate narrows as the unit correlates replies across successive interrogations (N = 0, 1, 2…). This is a King Radio DME patent, not a KDM 7000B drawing. Whether the KDM 7000B used this method is not known.
Figure 11. Sheet 1 of King Radio's US 4,599,617. Fig. 1 is the basic block diagram: clock, counter, latch, RAM and microprocessor (MPU), with decoded video from the receiver setting a flip-flop to capture each range count. Fig. 2 shows how the range gate narrows as the unit correlates replies across successive interrogations (N = 0, 1, 2…). This is a King Radio DME patent, not a KDM 7000B drawing. Whether the KDM 7000B used this method is not known.
Source: J. L. Stolpman, U.S. Patent 4,599,617 (assignee King Radio Corp.), 1986 [25]. U.S. patent drawings are public domain. Cropped and scaled.

The patent comes from the same company and location and dates from 1981–1986, a few years before the KDM 7000B service bulletins of 1988. It is reasonable to read it as evidence of how King's DME engineers worked, but not as a description of the KDM 7000B. The KDM 7000 predates the patent's 1981 filing by at least four years [2], so the basic 7000 at least cannot have been designed around it. Inferred

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6. Variants and part numbers

In briefAll KDM 7000 models share the base part number 066-1019; the dash number identifies the variant and configuration [5][10][1]. Sources name four versions: KDM 7000, 7000A, 7000B and a "KDM 7000B (521D)" [6]. Australia's airworthiness directive lists six KDM 7000B dash numbers [1]. A Boeing 747 manual gives new dash numbers for units modified to cure the false-channeling problem [4]. One dealer lists -21 as a "KDM-7000," which conflicts with the CASA directive [11][1].

Bendix/King's own training grouped the models: the author's January 1993 course was titled "KDM 7000/A/B Digital DME Theory & Maintenance" [29], consistent with the shared "KDM7000/A/B" assemblies in the parts catalog [6]. What distinguished the three models is still not documented Not found.

ModelWhat the sources showSource
KDM 7000Existed by Feb. 1977; "digital ARINC 568 DME Interrogator"; 066-1019-00 sold as "D.M.E." with alternate P/N KDM-7000; own maintenance manual 006-05027-0005[2][10][6]
KDM 7000A"DME Transceiver," 066-1019-xx; maintenance manual 006-05135-0001; installation manual 006-00135-0000[5][6]
KDM 7000B066-1019-xx; maintenance manual 006-05155-0005; installation manual 006-00155-0002; SBs KDM 7000B-34-12 and -34-14[5][6][7][1]
KDM 7000B (521D)Separate maintenance manual 006-05164-0001 and installation manual 006-00164-0000. A photo caption calls a unit a "KDM 7000B 521D DME." Probably the version for aircraft wired to the older ARINC 521D standard Inferred[6][14][22]
KDM 700 (earlier King DME, for comparison)P/N 066-1003-00; 11.4 lb; TSO C66 Cat B; 14 V dc 5.5 A or 28 V dc 2.75 A (museum data plate). A different, earlier King DME, not part of the 7000 family[27]

6.1 Dash numbers

Dash number(s)Identified asSourceNotes
066-1019-00KDM-7000 ("D.M.E.")[10]
066-1019-21, -23, -26, -33, -43, -57KDM 7000B (S/N 21855–22526 affected by the AD)[1]Confirmed
066-1019-21"KDM-7000 DME Transceiver"[11]Sources differ CASA calls -21 a KDM 7000B. The dealer listing is more likely a generic family label.
066-1019-27KDM 7000B (seller's data plate, last digits partly masked)[12]Seller text says "006-1019-27" (typo) Unverified
066-1019-ALLKDM 7000A and KDM 7000B[5]repair capability, all dashes
Boeing 747 AMM: modified part numbersafter the false-channeling fix; from an indexed excerpt

The Boeing 747 AMM excerpt warns that, when installing "Bendix KDM 7000/B DME interrogators," the part numbers must agree with its Table 1, and that with unmodified units paired with Collins 51RV-4 or King Radio KNR 6030 VHF NAV receivers "the NAV receiver may channel to a frequency other than the one on the control panel," which could cause flight path deviations. It cites Boeing SB 34A2308 for effectivity [4].

UnmodifiedModified
066-1019-00066-1019-05
066-1019-01066-1019-06
066-1019-21066-1019-61
066-1019-23066-1019-63
066-1019-24066-1019-64
066-1019-27066-1019-67
066-1019-28066-1019-68

Caution: the aero.cn page could not be loaded for this document; the table above comes from the search engine's indexed excerpt of it [4] Unverified. The pattern (add 40 to dashes in the 20s; add 5 to -00 and -01) is consistent, but it should be checked against a real AMM before relying on it. The table does not say which of these dashes are 7000 and which are 7000B; the CASA directive confirms -21 and -23 as 7000B [1].

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7. Indicator, control panel and antenna

In briefThe KDM 7000B has no controls or display of its own for the crew; it is a "remote" box. The crew-facing parts are the NAV control panel (which tunes it) and the DME indicators (which show the distance). ARINC 568 sets out what those units should do [22]. King made DME indicators called the KDI 5710 and KDI 5700, whose manuals are still catalogued [6], and the KDI 5710 is the indicator a shop needs to bench-test a KDM 7000B [8]. The specific indicator, control panel and antenna models used with the KDM 7000B on any given aircraft were not found.

UnitWhat ARINC 568 specifiesKDM 7000B-related evidenceSource
DME indicator"Standard distance indicator": 26 V ac power input, serial BCD input with isolation, defined display when data is absent or the equipment fails, indicator status output; electromechanical and light-bar typesKing KDI 5710 (maintenance manual 006-05025-0000) and KDI 5700 (006-05041-0000). KDI 5710 required with the ASI-776-4 test set. Unit P/Ns and cockpit use not confirmed[22][6][8]
Control panelCommon VHF NAV and DME frequency selectors; off-on and on-standby controls; 200-mile search-range-limit override switch; volume controls; ARINC 519 glide-slope frequency selection; integral lighting; two-out-of-five frequency codeNot identified. The 747 AMM ties the KDM 7000/B to Collins 51RV-4 and King KNR 6030 NAV receivers, which share its channeling[22][4]
AntennaImpedance and VSWR, gain and polarization, power rating, radiation pattern, antenna isolation; typical flush and blade antennasNot identified Not found[22]
Analog adapterAppendix 5: adapting ARINC 521D installations to accept ARINC 568 units; Attachment 4: deriving analog distance from the serial BCD outputKing 499 synchro driver (P/N 068-1013) for "compatibility with an analog ARINC 521D DME"[22][2]

The Honeywell Bendix King catalog also lists other "DME INDICATOR" part numbers, but none of the entries found names the KDI 5710 or KDI 5700 or links them to the KDM 7000B, so they are not listed here Not found. The KDI 572, 573 and 574 indicators in the same catalog belong to King's general-aviation DME line [6]; no source connects them with the KDM 7000B.

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8. Operation and maintenance

In briefIn the air, the crew had little to do with the KDM 7000B: tuning a VOR or ILS frequency tuned the DME, and the distance appeared on the indicator. In the shop, Bendix/King specified test set 696-2795-00; Avionics Specialist, Inc. builds an equivalent (ASI-776-4) that combines the test set and pin-out panel and works with a DME signal generator and a KDI 5710 indicator [8]. The KDM 7000B's best-documented event is the late-1988 false-channeling fix: Bendix/King Alert SB KDM 7000B-34-14 and FAA AD 88-25-01 [1][3].

8.1 In the cockpit

Because DME channels are paired with VHF NAV frequencies, the crew tuned the DME by tuning the NAV receiver; the KDM 7000B followed on the shared channeling lines [1][20]. They confirmed the station by its Morse identifier, heard as a 1350 Hz tone [18]. The ARINC 568 features the unit was built to include a "memory" that holds distance through short signal gaps, a warning flag on failure, a functional test, and 200 NM search-range limiting with an override [22]. Which of these a KDM 7000B installation used, and what its front-panel test did, was not found. Not found

8.2 Shop test equipment

ItemDetailsSource
Bendix/King 696-2795-00OEM KDM 7000 test set (OEM P/N as given by ASI)[8]
ASI-776-4 "KDM-7000 Test Set"Equivalent to 696-2795-00. Tests KDM-7000, 7000A and 7000B. Works with a DME indicator, a DME generator and standard shop equipment. Combines the DME test set and the pin-out panel in one unit. The KDI-5710 indicator is user-supplied; the interface cable is included. 12.25 × 19 × 12 in; 115 V ac 400 Hz. Supplied item ASI-77-64A[8]
ASI-176-1 (option)ARINC 568 DME indicator test set[8]
ASI-182 (option)Collins DME test set, 622-3582-001[8]
LinAire LA-3009, cable LD 8008Test-panel harness cable for the Honeywell KDM 7000/A/B[9]
"Top connector – for shop use only"Test connector on the unit itself (seen in a seller's photo)[12]
"860E 2 test rig"A photo caption shows a "KDM 7000B 521D DME with an 860E 2 Test rig." The 860E-2 is not identified further in the source[14] Unverified

8.3 Manuals

DocumentHoneywell/King P/NSource
KDM 7000 maintenance manual006-05027-0005[6]
KDM 7000A maintenance manual006-05135-0001[6]
KDM 7000A installation manual006-00135-0000[6]
KDM 7000B maintenance manual006-05155-0005[6]
KDM 7000B installation manual006-00155-0002[6]
KDM 7000B (521D) maintenance manual006-05164-0001[6]
KDM 7000B (521D) installation manual006-00164-0000[6]
KDI 5710 maintenance manual006-05025-0000[6]
KDI 5700 maintenance manual006-05041-0000[6]
King 499 synchro driver CMM 34-50-01 (Pacific Electro Dynamics, Feb. 1977)King 006-5153-00[2]
SB KDM 7000B-34-1260007439-0020 (subject not found)[7]

These are current catalog listings; which editions were in use in 1989–1996 is not known. No manual text was available for this document. Not found

8.4 The 1988 false-channeling directive

The most serious documented problem with the KDM 7000B involved its connection to the NAV receiver. Because the DME and the VHF NAV receiver were tuned over the same, paralleled channeling lines, a failure in the DME or its power supply could pull those lines to the wrong state, so the NAV receiver selected a different frequency from the one set on the control panel [1]. The Boeing 747 AMM warns that this "could cause flight path deviations" [4]. In the worst case a crew could follow guidance from a station other than the one they had selected. Inferred

DateActionDetailsSource
Nov. 4, 1988Bendix/King Alert SB KDM 7000B-34-14Modification of affected units[1]
Dec. 20, 1988FAA AD 88-25-01"Bendix/King Distance Measuring Equipment"; full text not found[3]
Feb. 1989CASA AD/RAD/45 (Australia)P/N 066-1019-21/-23/-26/-33/-43/-57, S/N 21855–22526. Fitted units: within 150 h time in service after Feb. 23, 1989 or before May 23, 1989, whichever is sooner; spare units: before fitment[1]
Not datedBoeing SB 34A2308 and 747 AMM warningPart numbers must agree with the AMM table; modified dashes -05, -06, -61, -63, -64, -67, -68[4] Unverified

The AD came out in December 1988, just before the author's 1989–1996 period of radar and DME work began, and about four years before his January 1993 KDM 7000/A/B course [29]. Units still awaiting modification could have been passing through shops in the early 1990s. Inferred

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9. Specifications

In briefOnly a handful of KDM 7000B-specific specifications are available, almost all from one data plate seen in a seller's photo: 18.3 lb, 115 V ac 400 Hz at 0.5 A, TSO-C66a [12]. Performance figures such as transmitter power, receiver sensitivity and accuracy were not found. The table separates what is known about this unit from the general DME and ARINC 568 figures that any compliant unit had to meet.

ItemValueSourceStatus
KDM 7000B-specific
TypeAirborne DME interrogator (transceiver); "digital ARINC 568"; Bendix/King course title "KDM 7000/A/B Digital DME"[1][2][4][29]Confirmed
MakerKing Radio Corp., Olathe, Kansas (data plate); Bendix/King (SB, AD); now Honeywell Bendix King catalog[12][1][3][6]Confirmed
Part number066-1019-xx; 7000B dashes -21, -23, -26, -33, -43, -57 (CASA); -27 (seller plate)[1][12]Confirmed Sources differ SEA lists -21 as "KDM-7000" [11]
Weight18.3 lb (8.3 kg Calculated)[12]Confirmed one data plate
Power115 V ac, 400 Hz, 0.5 A (about 58 VA apparent power at the plate rating Calculated)[12]Confirmed one data plate
CertificationTSO C66a; RTCA DO-160 environmental category (string only partly legible)[12]Confirmed
ConnectorsP7001 and P7002 on the rear; top-mounted shop test connector[12]Unverified from photos
AircraftBoeing 747; Boeing 737[4][12]Confirmed
Transmitter peak powerNot found—Not found
Receiver sensitivityNot found—Not found
AccuracyNot found—Not found
X/Y channel coverageNot found—Not found
Dimensions / ARINC case sizeNot found—Not found
Introduction dateNot found; KDM 7000 existed by Feb. 1977[2]Not found
Standard DME figures (apply to any DME)
Band960–1215 MHz; channels 962–1213 MHz[17][18][19]Confirmed
Interrogation frequencies1025–1150 MHz[19][21][17]Confirmed
Channels252: 126 X + 126 Y[17]Confirmed
Pulse spacingX: 12 µs both ways. Y: 36 µs interrogation, 30 µs reply. FAA Order 6820.14 gives 36 µs for Y without separating interrogation and reply Sources differ[17][19][20]Confirmed
Pulse width3.5 ± 0.5 µs[20]Confirmed
Ground reply delay50 µs (X), 56 µs (Y)[17][20]Confirmed
Time per NM≈12.36 µs round trip[19][20]Confirmed
Search / track rate≈150 pulse pairs/s search; ≤30 track (NRAO: 24–30)[19][20][21]Confirmed
System accuracyAIM: better than ½ NM or 3%, whichever is greater. ICAO recommendation: 0.25 NM + 1.25%[18][19][20]Confirmed Sources differ different measures
Usable rangeUp to 199 NM at line-of-sight altitude (AIM); ARINC 568 200 NM search-range limit[18][22]Confirmed
Ident tone1350 Hz Morse, about every 30 s[18][17]Confirmed
Airborne standardTSO-C66 (C66a on the plate; current revision C66c invokes RTCA DO-189)[12][24]Confirmed
Airline interfaceARINC 568: 6-wire serial, 32-bit words, ≈11 kHz clock[22][23]Confirmed
Notes on the conflictshow the disagreements were handled
  • 066-1019-21: KDM 7000B or KDM-7000? The CASA directive, a regulatory document that lists the -21 among "King model KDM 7000B" part numbers, is preferred over a dealer's product page [1][11]. Dealers often file every dash under the family name.
  • Y-channel spacing. FAA Order 6820.14 gives 36 µs as "the spacing for a Y-channel" [17]; Wikipedia and airnav.eu say 36 µs for interrogations and 30 µs for replies [19][20]. These agree once direction is taken into account.
  • Accuracy. The AIM figure (½ NM or 3%) is an operational statement for pilots; the ICAO figure (0.25 NM + 1.25%) is a system recommendation [18][19]. Neither is a KDM 7000B specification.
  • Seller part number "006-1019-27". Treated as a typo for 066-1019-27: the photographed plate shows "066-1019-" [12].
  • King Radio acquisition date. 1983 or 1985, depending on the source [15][14]. It does not affect the KDM 7000B story.

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10. Firsthand notes

In briefThe author's firsthand material for this unit is his certificate for Bendix/King's "KDM 7000/A/B Digital DME Theory & Maintenance" course of January 18–22, 1993 [29], together with his 1989–1996 period of radar and DME work. The rest of this page is drawn from the cited sources, not from his memory of the work.

Documented: training (Rick Childers) Firsthand
The author completed Bendix/King's KDM 7000/A/B Digital DME Theory & Maintenance course, January 18–22, 1993 (Allied-Signal Aerospace Company; form 058-02638-0001) [29]. Radar and DME work overall: 1989–1996. See the training certificate.

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11. Open research questions

In briefWhat the sources could not answer. The identity of the "7000B" is settled, and the author's January 1993 Bendix/King course certificate dates his training on it. The remaining gaps concern its internals and performance.

GapStatus / where to look
KDM 7000B introduction date; 7000A and 7000B datesNot found. KDM 7000 existed by Feb. 1977 [2]. King/Bendix-King catalogs or trade press of the late 1970s–1980s would help
Transmitter power, receiver sensitivity, accuracy, X/Y coverage, sizeNot found. KDM 7000B maintenance manual 006-05155-0005 or installation manual 006-00155-0002 [6]
Full list of cards (2, 5, power supply, transmitter)Not found in the catalog pages checked [6]
Full text of FAA AD 88-25-01 and SB KDM 7000B-34-14Only the dates and summary were found [3][1]
Subject of SB KDM 7000B-34-12Catalog title only [7]
Boeing 747 AMM tableOnly a search-engine excerpt; the page did not load [4]
Differences between 7000, 7000A, 7000B and 7000B (521D)Not found; the separate 521D manuals suggest a wiring-standard variant [6]
Indicator, control panel and antenna part numbers used with the KDM 7000BNot found
A freely licensed photo of a KDM 7000BNone found; only commercial listing photos (§12)
Current Honeywell support statusManuals and cards are still listed in the Honeywell Bendix King catalog [6]; whether Honeywell still repairs the unit was not established

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12. Photos found elsewhere

In briefNo freely licensed photograph of a KDM 7000B was found. These pages have photos that are commercial or otherwise restricted, so they are linked rather than reproduced. Listings can disappear at any time.

WhereWhat it showsLink
Whaletail Sales listing [12]KDM 7000B from a retired 737: front, rear connectors, top and data plate (4 photos). The best views found; the data plate readings in §3 come from thesewhaletailsales.com
SE Aerospace [11]KDM-7000 family product page (stock image)seaerospace.com
Flying Tin [14]Photo captioned "a KDM 7000B 521D DME with an 860E 2 Test rig," alongside other test equipmentflyingtin.com
Ingenium museum [27]King KDM 700, an earlier King DME, with data plate (non-commercial licence)collections.ingenium.ca
ILS Aviation Auctions [10]066-1019-00 "D.M.E." (KDM-7000) auction listingauction.ilsmart.com

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Glossary

In briefPlain-language definitions of the terms and abbreviations used in this document.

Airworthiness directive (AD)
A mandatory safety instruction from an aviation authority. FAA AD 88-25-01 and CASA AD/RAD/45 cover the KDM 7000B. [3][1]
AMM
Airplane maintenance manual: the aircraft manufacturer's manual for work on the aircraft, such as the Boeing 747 AMM chapter 34. [4]
ARINC 429
The later, widely used airliner data bus. Not the bus the KDM 7000B used (that was ARINC 568). [23]
ARINC 521D
An earlier airline DME standard with analog outputs. The King 499 synchro driver let an ARINC 568 KDM 7000 work in an aircraft wired for it. [2][22]
ARINC 568
The airline standard ("characteristic") for the Mark 3 airborne DME: box form factor, connectors, wiring, and a six-wire serial digital output of distance. King called the KDM 7000( ) a digital ARINC 568 interrogator. [22][2][23]
BCD
Binary-coded decimal: each decimal digit sent as a 4-bit code. ARINC 568 sends distance as serial BCD. [22]
Channeling
Selecting the DME channel. In the KDM 7000B installation the DME and VHF NAV receiver share paralleled channeling lines, the subject of AD 88-25-01. [1][4]
CMM
Component maintenance manual: the shop manual for one unit, organized by ATA chapter (34 for navigation). [2]
DO-160
RTCA's environmental test standard for airborne equipment. The data plate's "ENV CAT" string encodes the categories tested. [12]
Duplexer
A component that lets a transmitter and receiver share one antenna. The KDM 7000/A/B has a duplexer assembly. [6]
EE bay
Electrical and electronics equipment bay: the avionics compartment where remote units such as the KDM 7000B are installed. [4]
IF
Intermediate frequency: the fixed lower frequency a receiver converts signals to for amplification and detection. The KDM 7000/A/B has an IF board. [6]
ILS
Instrument landing system. DME channels are also paired with ILS localizer frequencies. [20][19]
Interrogator
The airborne half of DME: it sends pulse-pair interrogations and times the replies. The KDM 7000B is an interrogator. [17][4]
Jitter
Deliberately irregular spacing of interrogations, so each aircraft can recognize replies to its own interrogations among everyone else's. [25][20]
L band
The radio band around 1–2 GHz. DME (960–1215 MHz) sits at its lower end, alongside ATC transponders and TCAS. [17][19]
Preselector
A tuned filter ahead of a receiver that passes the wanted band and rejects strong out-of-band signals. A KDM 7000/A/B assembly. [6]
Pulse pair
Two pulses sent a fixed time apart (12 µs on X channels). DME always transmits in pairs; the spacing identifies the channel type. [17][20]
Range gate
A time window, centered on the expected reply time, in which a DME looks for its own replies. King's US 4,599,617 varies its width. [25]
Reply delay
The fixed time a ground station waits between receiving an interrogation and replying: 50 µs (X) or 56 µs (Y). The interrogator subtracts it. [17]
Service bulletin (SB)
A manufacturer's instruction to inspect or modify equipment. "Alert" bulletins address safety issues, such as SB KDM 7000B-34-14. [1]
Slant range
The straight-line distance from the aircraft to the ground station, which is what DME measures. It exceeds ground distance, most noticeably close to the station at altitude. [18]
Squitter
Pulse pairs a ground station transmits without being interrogated, keeping its output steady. Aircraft ignore them because they are not synchronous with their own interrogations. [17][20]
SSR
Secondary surveillance radar (ATC radar beacon system), which uses 1030 and 1090 MHz; DME assignments avoid those frequencies. [19][21]
Synchro
An electromechanical AC position transmitter/receiver used by older analog instruments. The King 499 "synchro driver" converted digital DME data for such installations. [2]
TACAN
The military tactical air navigation system; its distance function is compatible with civil DME. VOR + TACAN = VORTAC. [19][20]
Transponder (DME ground station)
The ground half of DME: it receives interrogations and replies after a fixed delay. Not to be confused with the aircraft's ATC transponder. [17]
TSO-C66
The FAA Technical Standard Order for airborne DME. The KDM 7000B plate says TSO C66a; the current revision, C66c, invokes RTCA DO-189. [12][24]
VCO
Voltage-controlled oscillator: an oscillator whose frequency is set by a control voltage, typically part of a frequency synthesizer. A KDM 7000/A/B assembly. [6]
VOR
VHF omnidirectional range: a ground beacon giving bearing. DME channels are paired with VOR frequencies, and many stations are VOR/DMEs. [18][19]
X and Y channels
The two families of 126 DME channels, differing in pulse spacing (X 12/12 µs, Y 36/30 µs) and reply delay (50 or 56 µs). [17][19][20]

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13. Image credits

In briefEvery image on this page is public-domain government or patent material, openly licensed material with a named author, or an original diagram drawn for this document. None shows an actual KDM 7000B; no commercial listing photos are embedded. The author's training certificate is shown on a separate companion page.

Image(s)SourceLicense
System interconnect; DME timing; channel plan; slant range; timeline; KDM 7000B assembly listOriginal diagrams drawn for this document from the cited sourcesOriginal work
DME two-way ranging conceptFAA Order 6820.14, Figure 2-2 [17]U.S. Government work, public domain
King Radio microprocessor DME, patent sheet 1J. L. Stolpman / King Radio Corp., US 4,599,617 [25]U.S. patent drawing, public domain
Boeing 737-200 flight deckQuintin Soloviev, 2024, via Wikimedia Commons [30]CC BY 4.0
Jet airliner antenna locationsTosaka, 2010, via Wikimedia Commons [31]CC BY-SA 3.0
DCA VOR/DME ground stationMediaGuy768, 2023, via Wikimedia Commons [32]CC BY-SA 4.0

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14. References

In briefAll sources cited in the text. URLs were checked in September 2026.

  1. [1]Civil Aviation Safety Authority (Australia), Airworthiness Directive AD/RAD/45, "King KDM 7000B Distance Measuring Equipment," issue 2/89 (applicability P/N 066-1019-21/-23/-26/-33/-43/-57, S/N 21855–22526; requires Bendix/King Alert Service Bulletin KDM 7000B-34-14 of 4 Nov. 1988; "FAA AD 88-25-01 refers"). https://services.casa.gov.au/airworth/airwd/ADfiles/equip/rad/rad-045.pdf
  2. [2]Essco Aircraft, listing for "King Synchro Driver Assembly Part No. 499 Component Maintenance with Parts 34-50-01" (Pacific Electro Dynamics CMM, Feb. 1977; King manual P/N 006-5153-00, King P/N 068-1013). The listing describes the 499 as used with a "King Radio Model KDM 7000( ) digital ARINC 568 DME Interrogator to provide compatibility with an analog ARINC 521D DME." https://www.esscoaircraft.com/products/king-synchro-driver-assembly-part-no-499-component-maintenance-with-parts-34-50-01
  3. [3]Air Research (airresearch.com), index of FAA appliance airworthiness directives, heading "Bendix/King": "88-25-01 Distance Measuring Equipment 12/20/88." https://www.airresearch.com/demo/appl.htm
  4. [4]Boeing 747 Airplane Maintenance Manual, Chapter 34 (Navigation), DME section, as reproduced by aero.cn. Warning that KDM 7000/B interrogators must match part numbers in the AMM table, with an unmodified-to-modified part-number table and reference to Boeing SB 34A2308. Note: the page timed out when fetched for this document; the content was read from the search engine's indexed excerpt. http://www.aero.cn/2011/0320/21820_100.html
  5. [5]Field Aviation East Ltd., Avionics Instruments and Components Capability List, report 400-068-90 Rev. 42 (lists 066-1019-ALL Bendix/King KDM 7000A "DME Transceiver" and KDM 7000B "DME"). https://fieldaero.com/Portals/0/ThemePluginPro/uploads/2024/4/25/400-068-90-r-42-avionics-instruments-and-components-capability-list.pdf
  6. [6]Honeywell Bendix King Product Reference Catalog (CAGE 01KG6), as indexed by Aeroval: manuals on pp. 87, 88, 106 and 107; KDM 7000/A/B circuit-card and module entries on pp. 1025–1026 (link is p. 1025; change "pg=" for the other pages). https://aeroval.com/ref/?pg=1025&search=bendix
  7. [7]Aeroval catalog entry 60007439-0020, "SB KDM 7000B-34-12" (Honeywell Bendix King service bulletin). https://aeroval.com/ref/2229324/60007439-0020/
  8. [8]Avionics Specialist, Inc. (ASI), ASI-776-4 "KDM-7000 Test Set," equivalent Bendix/King P/N 696-2795-00; units tested KDM-7000, KDM-7000A, KDM-7000B. https://www.asitest.com/cgi-bin/Results.pl?CatalogIndex=2939
  9. [9]LinAire LA-3009 test-panel harness cable list (as posted by Avionteq): cable "LD 8008 — Honeywell KDM 7000/A/B." http://www.avionteq.com/LinAire-LA-3009-Test-panel-harness-cable.aspx
  10. [10]ILS Aviation Auctions listing, "066-1019-00 – D.M.E.," alternate part number KDM-7000. https://auction.ilsmart.com/Listing/Details/1702515/066101900-DME
  11. [11]SE Aerospace, "066-1019-21 BendixKing KDM-7000" parts listing. https://www.seaerospace.com/sales/product/BendixKing/KDM-7000/066-1019-21
  12. [12]Whaletail Sales, "KDM 7000B DME" listing ("from retired 737 aircraft"; text gives "PN:006-1019-27"), with four photos including the data plate. Photos are the seller's and are not reproduced here. https://whaletailsales.com/products/kdm-70008-dme
  13. [13]Aircraft Parts Store, "P/N 076-00340-0001 – TUNING MEC KDM7000." https://aircraftpartsstore.com/shop/product/076-00340-0001
  14. [14]Flying Tin editorial team, "Silver Crown: The History of King Radio," July 5, 2026 (includes a photo captioned "a KDM 7000B 521D DME with an 860E 2 Test rig"). https://www.flyingtin.com/industry/silver-crown-the-history-of-king-radio-4174/
  15. [15]Wikipedia, "King Radio (company)." https://en.wikipedia.org/wiki/King_Radio_(company)
  16. [16]Wikipedia, "AlliedSignal." https://en.wikipedia.org/wiki/AlliedSignal
  17. [17]Federal Aviation Administration, Order 6820.14, Siting Criteria for Distance Measuring Equipment, Oct. 19, 2023, Chapter 2 "The DME System" (Figure 2-2 "DME Two-way Ranging Concept"; U.S. Government work). https://www.faa.gov/documentLibrary/media/Order/FAA_Order_6820.14.pdf
  18. [18]Federal Aviation Administration, Aeronautical Information Manual, Chapter 1, Section 1, paragraphs 1-1-7 "Distance Measuring Equipment (DME)" and 1-1-8 "Navigational Aid (NAVAID) Service Volumes." https://www.faa.gov/air_traffic/publications/atpubs/aim_html/chap1_section_1.html
  19. [19]Wikipedia, "Distance measuring equipment." https://en.wikipedia.org/wiki/Distance_measuring_equipment
  20. [20]airnav.eu, "DME Infographics" (channel pairing table, pulse characteristics, X/Y spacing and delay table, search/track rates; cites ICAO Annex 10 Vol. I §3.5). http://www.airnav.eu/index.php?stranka=DMEen
  21. [21]National Radio Astronomy Observatory, Electronics Division Internal Report 313 (DME band: air-to-ground 1025–1150 MHz, ground-to-air 962–1024 and 1151–1213 MHz; 150 pulse pairs/s search). https://library.nrao.edu/public/memos/edir/EDIR_313.pdf
  22. [22]ARINC Characteristic 568, Mark 3 Airborne Distance Measuring Equipment (table of contents as published by Intertek Inform for Supplement 8; withdrawn 2013). https://www.intertekinform.com/en-au/standards/arinc-568-68-supp-8-98479_saig_arinc_arinc_207002/
  23. [23]North Atlantic Industries, Model AR2 ARINC 568/582 interface description (six-wire serial bus; 32-bit words with an 8-bit label). https://www.naii.com/model/AR2
  24. [24]RTCA DO-189 (1985), Minimum Operational Performance Standards for Airborne Distance Measuring Equipment (DME) Operating within the Radio Frequency Range of 960–1215 Megahertz (catalog listing). FAA TSO-C66c invokes DO-189. https://store.accuristech.com/standards/rtca-do-189?product_id=2200277
  25. [25]J. L. Stolpman (assignee King Radio Corporation, Olathe, Kansas), U.S. Patent 4,599,617, "Method and apparatus for evaluating the range data accumulated by distance measuring equipment," filed Sept. 21, 1984 (continuation of an application filed June 19, 1981), issued July 8, 1986. https://patents.google.com/patent/US4599617A/en
  26. [26]Earlier King Radio Corp. DME patents cited by US 4,599,617: US 3,412,400 "Method and apparatus for digitally measuring distance" (filed 1966, issued 1968); US 3,456,257 "…rapid search distance measuring equipment" (1967/1969); US 3,533,060 "Indicator for distance measuring equipment" (1966/1970); US 3,702,475 "Search-track decision circuit for distance measuring equipment" (1970/1972). Link is US 3,702,475. https://patents.google.com/patent/US3702475A/en
  27. [27]Ingenium – Canada's Museums of Science and Innovation, artifact 2005.0212.001, King KDM 700 DME (data plate: P/N 066-1003-00, WT 11.4 lbs, TSO C66 Cat B, 14 V dc 5.5 A / 28 V dc 2.75 A). Museum image licence is non-commercial, so it is linked, not reproduced. https://collections.ingenium.ca/en/id/2005.0212.001/
  28. [28]Precision Aero Technology (Precision Aviation Group), Commercial Capabilities catalog, Mar. 2024 (lists "2041167 (SERIES) DMA-37A DME XCVR, Honeywell," ATA 34, on 737, 747, 757, 767 and A320). https://www.precisionaviationgroup.com/wp-content/uploads/2024/03/PAT-Commercial-Catalog.pdf
  29. [29]Course completion certificate: "KDM 7000/A/B Digital DME Theory & Maintenance," presented by Bendix/King, Allied-Signal Aerospace Company, January 18–22, 1993 (form 058-02638-0001). Issued to the author; scan from the author's personal collection, supplied September 2026. Primary source; not published online.
  30. [30]Wikimedia Commons, "Inside of a Boeing 737-200 cockpit (Canadian North Airlines C-GDPA).jpg," photo by Quintin Soloviev, Oct. 17, 2024, CC BY 4.0. https://commons.wikimedia.org/wiki/File:Inside_of_a_Boeing_737-200_cockpit_(Canadian_North_Airlines_C-GDPA).jpg
  31. [31]Wikimedia Commons, "Jet-liner's antennas.PNG," drawing by Tosaka, Apr. 20, 2010, CC BY-SA 3.0 (legend item 5 = DME). https://commons.wikimedia.org/wiki/File:Jet-liner%27s_antennas.PNG
  32. [32]Wikimedia Commons, "DCA-VOR-DME.jpg," photo by MediaGuy768, Dec. 1, 2023, CC BY-SA 4.0. https://commons.wikimedia.org/wiki/File:DCA-VOR-DME.jpg

Written by Rick Childers, September 2026, for GeeksForge Research Projects. Firsthand material: the author's January 1993 training certificate and his 1989–1996 dates. Specifications are quoted from the sources shown; where sources disagree, both values are given.

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