Additional Information for Static Tube Mast
Static Tube Mast is a component of the Flight Instruments supply class in the Instruments And Laboratory Equipment supply group. It is used in aviation to measure static pressure, which is the atmospheric pressure exerted on an aircraft when it is not in motion. The static tube mast is typically mounted on the exterior of the aircraft and consists of a tube that is open at one end and connected to a pressure sensor at the other end. The open end of the tube faces into the airflow, allowing it to measure the static pressure accurately. This information is then used by the flight instruments to provide important data for the pilot, such as altitude and airspeed.
Related Item Names for INC 61825 Static Tube Mast
Airspeed-Altitude Computer Present Position Computer Pressure Altimeter Venturi Tube Attitude Indicator Turn And Slip Indicator Pitot Tube Pitot-Static Tube Static Tube Mach And True Air Speed Indicator Vertical Velocity Indicator Machmeter Air Speed Computer Mechanical Accelerometer Aircraft Inclinometer Aircraft Instruments Manifold Position Transmitter Position Indicator Recorder Subassembly Recorder Group Altitude Computer Azimuth-Elevation Deviation Indicator Control Surfaces Trim Indicator Data Display Group Course Indicator Linear Electrical Accelerometer Optical Element Cell Dummy Static Tube Indicator Housing Angle Of Attack Transmitter Flight Director Computer Air Data Computer Mach Number Computer Magnetic Recording Tape Reel Airspeed And Direction Indicator Computer Subassembly Head-Up Display Unit Air Speed Indicator Angle Indicator Gyroscopic Heading Indicator Airport Runway Instrument Landing Indicator Instruments And Laboratory Equipment Modification Kit Wrist Instrument Strap Flight Data Recorder Collision Avoidance Computer Data Acquisition Unit Head-Up Display Symbol Generator Head-Up Display Monitor Pressure Altimeter Subassembly Automatic Pressure Standby Servo Controlled Altimeter Subassembly Preset Command Information Servo Controlled Altimeter Subassembly Air Speed Indicator Subassembly Flight Instruments Angle Indicator Subassembly Attitude Indicator Subassembly Flight Instruments Course Indicator Subassembly Gyroscopic Heading Indicator Subassembly Mach And True Air Speed Indicator Subassembly Flight Instruments Position Indicator Subassembly Control Surfaces Trim Indicator Subassembly Turn And Slip Indicator Subassembly Vertical Velocity Indicator Subassembly Flight Data Recorder Interface Subassembly Flight Data Recorder Memory Unit Electronic Air Inlet Controller Flight Information Processor Fuel Management Computer Flight Information Display Unit Fuel Management Panel Fuel Savings Advisory Computer Ground Speed Indicator Control-Display Unit Static Tube To Case Section Adapter Automatic Pressure Standby Servo Controlled Altimeter Preset Command Information Servo Controlled Altimeter Stabilization Data Indicator Static Tube Protector Static Tube Subassembly Static Tube Base Static Tube Mast Static Tube Probe Static Tube Vane Assembly Multiple Aircraft Parameters Display Computer Multiple Aircraft Parameters Display Attitude And Heading Reference Unit Aircraft Pitot Static Drain Bottle Special Purpose Computer System Special Purpose Computer Autopilot Control Unit Impact Pressure Transducer
NATO Stock Numbers with Item Name 61825 Static Tube Mast Page 1 of 1
- 50-324150-93
- RNCC: 3 | RNVC: 2 | DAC: 1
- 260-04-34-1
- RNCC: 3 | RNVC: 2 | DAC: 1
- 2FJE03001-0004
- RNCC: 3 | RNVC: 2 | DAC: D
- 272D6271055
- RNCC: 3 | RNVC: 2 | MEDALS: Y | DAC: 2
- 23356-1
- RNCC: 3 | RNVC: 2 | DAC: 5
- 260-04-34-1
- RNCC: 3 | RNVC: 2 | DAC: 3
- 215-51062-2
- RNCC: 3 | RNVC: 2 | DAC: 2
- DHC60207-29
- RNCC: 3 | RNVC: 2 | DAC: 2
- 6610-0001
- RNCC: 6 | RNVC: 9 | DAC: 9