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Tu-214PU-SBUS Airborne Communication Station. First flight: 2017 (2018) © UAC
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Status: in service
Number built: 2
The two-letter initials “PU” – Flying command post
Abbreviation “SBUS” - “Special Onboard Communication Centre”
Registration: RA 64529 and RA 64530
Subordination: The Special Air Group for the Ministry of Defense of the Russian Federation


The aircraft was developed to provide communications between command and the Supreme Military Staff, including the President of Russia, in the event of hostilities and emergencies.
The aircraft carries a special SBUS-214 communication node (installed in front of the vertical stabilizer, in a special aerodynamic fairing on the upper part of the fuselage in which it is believed to be housed).

 

Tu-214PU-SBUS Airborne Communication Station © Konstantinos Panitsidis
Tu-214PU-SBUS Airborne Communication Station.

 


Three-view drawing

Tu-214PU-SBUS © Konstantinos Panitsidis

 

 


Technical specifications

DESIGNER OKB Tupolev
COUNTRY Russia
TYPE
Airborne Communication Station
CREW -
POWER-PLANT Two turbofan engines PS-90A
Thrust, kgf 2x16.000
DIMENSIONS
 
Length, m
46,20
Height, m
13,90
Wing span, m
42,00
Wing area, m2
182,40
WEIGHT  
Maximum take-off, kg 110.750
Normal take-off, kg -
Empty aircraft, kg 59.000
Internal fuel, kg -
Warload, kg -
PERFORMANCE  
Maximum speed, km/h -
Cruising speed, km/h 850
Range, km 6.500
Ferry range, km until 10.500
Service ceiling, m 12.000
Maximum overload, g -
ARMAMENT Doesn't have (defensive).