Website:
PBS VELKA BITES
Catalog excerpts
AUXILIARY POWER UNIT SAFIR 5K/G Z8 Designed for electrical starting of the main engine of helicopter
Open the catalog to page 1
Main parameters Rated electrical power Electrical power supply Fuel consumption Range of operation Main features H=0 m T=15 °C 40 kVA 3× 115 V/200 V max. 55 kg/hour −55 °C ÷ + 60 °C 0 ÷ 6,000 m • Continuous operation lasting 6 hours • High reliability of APU operations • Long service life and operation periods • Simple maintenance • Ecological fuel drainage Dimensions and weight Lenght (without AC generator) Width × Depth Weight (without AC generator) (including air inlet and air bleed system) • Unlimited number of main engine starts • Start and operation altitude up to 6,000 m Standard...
Open the catalog to page 2All PBS VELKA BITES catalogs and technical brochures
-
PBS JOURNAL9 Pages
-
PBS_APU Safir 5L2 Pages
-
PBS_APU_Safir 5 KG-MI-402 Pages
-
PBS APU Safir 5KG Z82 Pages
-
PBS Turbojet engine TJ40-G22 Pages
-
PBS Turbojet engine TJ802 Pages
-
PBS Turbojet engine TJ1002 Pages
-
PBS Turbojet engine TJ1502 Pages
-
PBS Turboshaft engine TS1002 Pages
-
PBS ECS systems2 Pages
-
PBS ECS-M1V2 Pages
-
PBS Starter-generator2 Pages
-
Two-channel Ignition Device8 Pages
-
PBS_Turbine blades catalogue16 Pages
-
PBS Turbine Blades2 Pages
-
PBS Spinner discs2 Pages
-
PBS Precision Casting4 Pages
-
PBS KNEE REPLACEMENTS2 Pages
-
SAFIR 5L2 Pages
-
SAFIR 5K/G MIS2 Pages
-
TJ80 TURBOJET ENGINE2 Pages
-
TS-100-turboshaft-engine2 Pages
-
TP-100-turbopropeller-engine2 Pages
-
TJ-100-turbojet-engine2 Pages
-
TJ-40-G2-Turbojet-Engine2 Pages
-
TJ-40-G1-Turbojet-Engine2 Pages
