EFIS control panel
$4125
EFIS control panel
Partner Stock
071-01439-3100 is the exact Part Number of this BendixKing CP 467 electronic flight instrument system control panel. The unit gives the flight crew a dedicated interface for selecting supported EFS 40/50 display presentations and reference functions. Its front panel combines course and heading controls with HSI, ARC and NAV presentation keys, range selection and system-reference controls in a compact cockpit-mounted assembly.
The CP 467 is a command panel rather than a flight-data sensor or display. It does not independently calculate heading, course, radio altitude or navigation position. Crew selections are passed to the compatible EFIS equipment, which processes data from the installed navigation and attitude sources and presents the resulting information on the electronic displays. The complete -3100 suffix is essential because CP 467 configurations can differ in lighting, faceplate and modification standard.
The HSI, ARC and NAV keys select the supported display formats within the approved EFS installation. The CRS control is used for course-related selection, while the HDG control provides heading-reference input. Range-up and range-down keys change the displayed scale where the connected system supports that command. The 1-2 key is used for the installed dual-source arrangement defined by the aircraft wiring and EFIS configuration.
RALT, SYS and REF controls provide access to the associated reference or system functions available in the installation, and the TST control supports the approved test sequence. A key label does not prove that every function is enabled on every aircraft. The installed symbol generators, displays, sensors, software configuration and wiring determine which selections are available and how they are annunciated to the crew.
Published equipment information identifies CP 467 as a control-panel option for Bendix/King EFS 40 and EFS 50 systems. A typical functional path is crew command at the CP 467, control data into the EFIS processing and display equipment, and presentation on compatible electronic attitude or horizontal-situation displays. Navigation receivers, heading references and radar-altitude sources remain separate associated units.
A documented MD 900-series optional-equipment installation uses two CP 467 panels with EFS 50 displays, including ED 551A electronic displays and ED 102 inclinometer-equipped attitude display installations. This is a confirmed example of system use, not a universal aircraft applicability statement. Eligibility for another aircraft must be established from its approved equipment list, wiring diagrams and current installation data.
The photographed 071-01439-3100 unit has a black faceplate and an original identification plate showing CP 467, TSO C113 and RTCA/DO-160B references. Partner documentation identifies HIRF-related configuration and 5 VAC, 5 VDC and 28 VDC lighting provisions for this exact listing. The applicable lighting connection must be verified against the aircraft wiring rather than inferred from faceplate appearance.
Receiving inspection should compare the full Part Number, serial number, modification marks, connector, mounting flange, controls and lighting configuration with the purchase order. Bench testing should confirm each key and rotary control, illumination, test function and interface output using approved maintenance data. The mating connector, mounting hardware, wiring and associated EFIS units are supplied only when expressly listed in the quotation.
This 071-01439-3100 CP 467 is offered in Serviceable condition from partner stock with a six-month warranty. The main image presents the control layout, while the authentic gallery image shows the original Part Number plate and rear connector. The photographed serial number is an identification reference and is not a promise that the same serial-numbered unit will be allocated unless confirmed in the quotation.
For an inquiry, specify Part Number 071-01439-3100, model CP 467, aircraft type, EFS 40 or EFS 50 configuration, lighting requirement, modification standard, required release documentation and quantity. Related EFIS, communication and navigation equipment can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related equipment may share one avionics suite but is not automatically interchangeable.
Product Type: Electronic flight instrument system control panel
Manufacturer: BendixKing / Honeywell
Model: CP 467
Designation: 071-01439-3100
Alternative Designations: CP467; CP-467; 071014393100; Bendix/King CP 467
Main Function: Crew selection of compatible EFIS display, course, heading, range and reference functions
System: Compatible Bendix/King EFS 40 / EFS 50 electronic flight instrument installations
Display Selection Controls: HSI, ARC and NAV
Range Controls: Range increase and decrease keys
Reference Controls: CRS, HDG, RALT, SYS and REF
Additional Controls: TST and 1-2 source-selection key as configured
Faceplate: Black configuration shown on the exact unit
Lighting Provisions: 5 VAC / 5 VDC / 28 VDC according to the exact partner listing; verify aircraft wiring
Qualification References: TSO C113 and RTCA/DO-160B according to the exact identification plate
Rear Interface: Multi-pin aircraft-system connector
Typical Signal Chain: CP 467 crew commands → EFIS processing / symbol generation → compatible electronic displays
Associated Equipment: EFS displays, symbol generators, navigation receivers, heading reference and radar-altitude equipment as installed
Documented Installation Example: MD 900-series optional EFS 50 installation with CP 467 and ED 551A equipment
Aircraft Applicability: Confirm from the aircraft equipment list and approved installation data
Exact Dimensions: Refer to the applicable CP 467 installation drawing
Weight: Reliable suffix-specific data were not confirmed in the reviewed open sources
Interchangeability: Full suffix, lighting, modification status, connector and system configuration must match
Condition: Serviceable
Warranty: 6 Months
Technical Documentation: Applicable Bendix/King EFS 40/50 and CP 467 installation and maintenance data
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.
071-01439-3100 is the exact Part Number of this BendixKing CP 467 electronic flight instrument system control panel. The unit gives the flight crew a dedicated interface for selecting supported EFS 40/50 display presentations and reference functions. Its front panel combines course and heading controls with HSI, ARC and NAV presentation keys, range selection and system-reference controls in a compact cockpit-mounted assembly.
The CP 467 is a command panel rather than a flight-data sensor or display. It does not independently calculate heading, course, radio altitude or navigation position. Crew selections are passed to the compatible EFIS equipment, which processes data from the installed navigation and attitude sources and presents the resulting information on the electronic displays. The complete -3100 suffix is essential because CP 467 configurations can differ in lighting, faceplate and modification standard.
The HSI, ARC and NAV keys select the supported display formats within the approved EFS installation. The CRS control is used for course-related selection, while the HDG control provides heading-reference input. Range-up and range-down keys change the displayed scale where the connected system supports that command. The 1-2 key is used for the installed dual-source arrangement defined by the aircraft wiring and EFIS configuration.
RALT, SYS and REF controls provide access to the associated reference or system functions available in the installation, and the TST control supports the approved test sequence. A key label does not prove that every function is enabled on every aircraft. The installed symbol generators, displays, sensors, software configuration and wiring determine which selections are available and how they are annunciated to the crew.
Published equipment information identifies CP 467 as a control-panel option for Bendix/King EFS 40 and EFS 50 systems. A typical functional path is crew command at the CP 467, control data into the EFIS processing and display equipment, and presentation on compatible electronic attitude or horizontal-situation displays. Navigation receivers, heading references and radar-altitude sources remain separate associated units.
A documented MD 900-series optional-equipment installation uses two CP 467 panels with EFS 50 displays, including ED 551A electronic displays and ED 102 inclinometer-equipped attitude display installations. This is a confirmed example of system use, not a universal aircraft applicability statement. Eligibility for another aircraft must be established from its approved equipment list, wiring diagrams and current installation data.
The photographed 071-01439-3100 unit has a black faceplate and an original identification plate showing CP 467, TSO C113 and RTCA/DO-160B references. Partner documentation identifies HIRF-related configuration and 5 VAC, 5 VDC and 28 VDC lighting provisions for this exact listing. The applicable lighting connection must be verified against the aircraft wiring rather than inferred from faceplate appearance.
Receiving inspection should compare the full Part Number, serial number, modification marks, connector, mounting flange, controls and lighting configuration with the purchase order. Bench testing should confirm each key and rotary control, illumination, test function and interface output using approved maintenance data. The mating connector, mounting hardware, wiring and associated EFIS units are supplied only when expressly listed in the quotation.
This 071-01439-3100 CP 467 is offered in Serviceable condition from partner stock with a six-month warranty. The main image presents the control layout, while the authentic gallery image shows the original Part Number plate and rear connector. The photographed serial number is an identification reference and is not a promise that the same serial-numbered unit will be allocated unless confirmed in the quotation.
For an inquiry, specify Part Number 071-01439-3100, model CP 467, aircraft type, EFS 40 or EFS 50 configuration, lighting requirement, modification standard, required release documentation and quantity. Related EFIS, communication and navigation equipment can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related equipment may share one avionics suite but is not automatically interchangeable.
Product Type: Electronic flight instrument system control panel
Manufacturer: BendixKing / Honeywell
Model: CP 467
Designation: 071-01439-3100
Alternative Designations: CP467; CP-467; 071014393100; Bendix/King CP 467
Main Function: Crew selection of compatible EFIS display, course, heading, range and reference functions
System: Compatible Bendix/King EFS 40 / EFS 50 electronic flight instrument installations
Display Selection Controls: HSI, ARC and NAV
Range Controls: Range increase and decrease keys
Reference Controls: CRS, HDG, RALT, SYS and REF
Additional Controls: TST and 1-2 source-selection key as configured
Faceplate: Black configuration shown on the exact unit
Lighting Provisions: 5 VAC / 5 VDC / 28 VDC according to the exact partner listing; verify aircraft wiring
Qualification References: TSO C113 and RTCA/DO-160B according to the exact identification plate
Rear Interface: Multi-pin aircraft-system connector
Typical Signal Chain: CP 467 crew commands → EFIS processing / symbol generation → compatible electronic displays
Associated Equipment: EFS displays, symbol generators, navigation receivers, heading reference and radar-altitude equipment as installed
Documented Installation Example: MD 900-series optional EFS 50 installation with CP 467 and ED 551A equipment
Aircraft Applicability: Confirm from the aircraft equipment list and approved installation data
Exact Dimensions: Refer to the applicable CP 467 installation drawing
Weight: Reliable suffix-specific data were not confirmed in the reviewed open sources
Interchangeability: Full suffix, lighting, modification status, connector and system configuration must match
Condition: Serviceable
Warranty: 6 Months
Technical Documentation: Applicable Bendix/King EFS 40/50 and CP 467 installation and maintenance data
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.