ASU-600-150-CUP: STARTER,ENGINE,AIR TURBINE.
The STARTER,ENGINE,AIR TURBINE is a the manufacturer industrial component. Key specifications include width: 60.0 INCHES NOMINAL IN, length: 167.1 INCHES NOMINAL IN, air_supply_flow_rate: 68.0 KILOGRAMS PER MINUTE KG, document_identification: ASU-600-150-CUP, standard_mounting_feature: INCLUDED. This part is cataloged in the U.S.
Government catalog under NSN 2995-01-729-5258, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| width | 60.0 INCHES NOMINAL IN |
| length | 167.1 INCHES NOMINAL IN |
| air_supply_flow_rate | 68.0 KILOGRAMS PER MINUTE KG |
| document_identification | ASU-600-150-CUP |
| standard_mounting_feature | INCLUDED |
| NSN | 2995-01-729-5258 |
| LENGTH | 167.1 INCHES NOMINAL IN |
| AIR SUPPLY FLOW RATE | 68.0 KILOGRAMS PER MINUTE KG |
| STANDARD MOUNTING FEATURE | INCLUDED |
| DOCUMENT IDENTIFICATION | ASU-600-150-CUP |
| SPECIAL FEATURES | JET START UNIT MAIN COMPONENTS ARE: CUMMINGS QSC ENGINE WITH ELECTRONIC CONTROL SYSTEM; ELECTRONIC CONTROL MODULE; OIL SENSORS; COOLANT AND TEMPERATURE LEVEL SENSORS; AIR INTAKE FILTER; EXHAUST SYSTEM; COMPRESSOR; OIL PRESSURE AND TEMPERATURE SWITCH; DELIVERED AIR SYSTEM; THROTTLE CONTROL; AIRCRAFT PROTECTION DEVICES |
| WIDTH | 60.0 INCHES NOMINAL IN |