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PNP-72-4M

Plan Navigation Indicator

AvailabilityIn stock
Availability
In stock
Condition
New
Warranty
6 Months
$5850

Description

PNP-72-4M in the aircraft navigation display system

The PNP-72-4M is a plan navigation indicator used in aircraft and helicopter flight-navigation complexes. It is a combined electromechanical cockpit instrument similar in function to an HSI — Horizontal Situation Indicator. The unit receives signals from onboard navigation sensors and systems, then converts them into movement of pointers, flags and scales on the front panel. In flight, the PNP-72-4M gives the crew a clear visual picture of heading, selected course, bearing, distance and deviation from navigation channels.

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Navigation functions of the PNP-72-4M

The PNP-72-4M combines the functions of several separate instruments in one housing. It works as a heading indicator, radio magnetic indicator, distance indicator and bearing / course deviation indicator. The pilot can monitor current heading on the rotating compass card, selected course, preset track angle, bearing to a navigation station, range to the selected ground station and deviation from the required course or glide path. This makes the instrument useful during route navigation, approach and operation with radio navigation systems.

PNP-72-4M as an electromechanical HSI-type instrument

The PNP-72-4M is not a digital screen. It is an analog electromechanical indicator with internal follow-up mechanisms. Signals from navigation systems are transmitted to the instrument and displayed through moving mechanical elements. This type of design is typical for Soviet and Russian aircraft cockpits where classic navigation information is shown through precise electromechanical instruments. Because of this, correct power supply, signal compatibility and smooth operation of the moving parts are critical for reliable indication.

Displayed data and warning flags on PNP-72-4M

The instrument displays the aircraft’s current heading, selected heading, bearing to radio beacons, course deviation, glide path deviation and distance information depending on the connected systems. It can also include warning flags, or blinker flags, that appear when certain connected navigation channels fail or become unreliable. These may relate to course, glide path, dead reckoning or other navigation inputs depending on the aircraft configuration. For the crew, these flags are important because they quickly show that a specific indication should not be trusted.

PNP-72-4M in flight and approach operation

During en-route flight, the PNP-72-4M helps the pilot maintain the required heading and monitor deviation from the selected route. When used with radio navigation equipment, it shows direction to a beacon and distance to a selected station. During approach, when connected to landing systems such as ILS or SP-50-type equipment, the instrument can show course and glide path deviation. The exact indication logic depends on the installed flight-navigation complex, but the role of the PNP-72-4M remains the same: to present key horizontal navigation data in one cockpit instrument.

Aircraft application of PNP-72-4M

The PNP-72 series is used on various Soviet and Russian aircraft and helicopters equipped with compatible flight-navigation systems. The PNP-72-4M may be found on helicopter and aircraft platforms where a combined plan navigation display is required, including Mi-8 series helicopters and other aircraft types depending on modification and equipment configuration. Before installation or replacement, the unit must be checked against the aircraft equipment list, wiring diagram, connector type, power supply and navigation system version.

Supply and service checks for PNP-72-4M

For supply, the full designation PNP-72-4M should be used. The instrument should be checked not only by appearance, but also by functional condition. Important inspection points include the front panel, connector, housing sealing, compass card movement, pointer response, warning flags, distance indication, backlighting and absence of sticking or jerky movement. Since the instrument works with several power channels and analog input signals, it should be accepted according to passport, bench test results and applicable aircraft documentation.

Related instruments: PNP-72-12, PNP-72-14, PNP-72-15. These links are grouped by type and system and do not indicate interchangeability.

Technical details

Designation
PNP-72-4M
Russian Designation
ПНП-72-4М
Function
Display of horizontal navigation data, heading, bearing, range and course / glide path deviation
Application / Where Used
Aircraft and helicopter flight-navigation complexes
All specificationsCollapse specifications
System / Installation Area
Cockpit instrument panel
Part of System / Included in Set
Flight-navigation complex / navigation indication equipment
Instrument Type
Electromechanical, analog, remote-following navigation indicator
Functional Equivalent
HSI-type aircraft navigation indicator
Displayed Parameters
Current heading, selected heading, preset track angle, drift angle, current azimuth, radio bearing, distance to selected station, course and glide path deviation
Warning Indication
Blinker flags for failure or unreliability of connected navigation channels, depending on aircraft configuration
Compatible Aircraft / Equipment
Mi-8 series helicopters, Su-25, L-39 and other aircraft equipped with compatible PNP-72 series navigation systems, depending on modification
Related Navigation Systems
Flight-navigation complexes, radio navigation systems, ILS / SP-50-type landing systems, Kurs-MP-type equipment depending on aircraft configuration
Front Panel Size
120 × 120 mm
Mounting Depth / Length
225 mm
Weight
Not more than 3.6 kg
DC Power Supply
27 V
Three-Phase AC Power Supply
36 V, 400 Hz
Lighting Supply
5.5 V AC or DC
Current and Selected Heading Indication Error
Not more than ±1°
Preset Track Angle Indication Error
Not more than ±1°
Drift Angle Indication Error
Not more than ±1°
Current Azimuth Indication Error
Not more than ±1°
Distance Indication Error, 0–499 km Range
Not more than ±1.5 km
Distance Indication Error, 0–999 km Range
Not more than ±3 km
Course / Glide Path Zone Deviation Error
Not more than 10%
Operating Mode
Continuous operation as part of the onboard flight-navigation complex
Construction Features
Sealed metal housing, vibration-resistant cockpit instrument design
Environmental Resistance
Designed for onboard vibration, linear acceleration loads and pressure changes during altitude operation
Technical Documentation
Product passport, wiring diagram and aircraft operating documentation as applicable

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PNP-72-4M