FSC 6610 Flight Instruments
Includes Air Speed Indicators; Rate of Climb Indicators; Bank and Turn Indicators; Pitot Tubes; Gyro Horizon Indicators; Attitude Gyro Indicators. Excludes Navigational Instruments (FSC 6605).
Name | NSN | Details | |
---|---|---|---|
Indicator,attitude | 6610-01-502-8510 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Indicator,attitude | 6610-00-000-0192 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Computer Subassembly | 6610-01-502-8868 | Two or more different types of items, having a common mounting or mounted on each other which together form a portion of a computer, but which in itself is not a complete functioning item and cannot be assigned a more definite item name. | RFQ |
Link,altimeter | 6610-00-001-2511 | RFQ | |
Flag Assembly,altim | 6610-00-001-2512 | RFQ | |
Altimeter,pressure | 6610-01-502-9907 | A barometric type instrument which measures altitude above a given datum plane when adjusted to the correct altimeter setting number. Excludes ALTIMETER, SURVEYING. | RFQ |
Venturi Tube | 6610-01-503-0153 | A device designed to provide a source of air for the operation of air-driven instruments. For items designed for liquid flow, see VENTURI METER. | RFQ |
Counter Bracket Ass | 6610-00-001-5508 | RFQ | |
Computer,air Data | 6610-01-503-2253 | A computer specifically designed to convert basic air data input signals into electrical output signals representing the necessary flight parameters such as pressure altitude, mach number, airspeed, and impact pressure. See also COMPUTER, AIR SPEED; COMPUTER, ALTIMETER-PRESSURE; COMPUTER, ALTITUDE; COMPUTER, MACH NUMBER; COMPUTER, PRESSURE-ALTITUDE; COMPUTER, TRUE WIND DIRECTION AND INTENSITY; and COMPUTER, ZONE WIND. | RFQ |
Computer,air Data | 6610-01-503-2254 | A computer specifically designed to convert basic air data input signals into electrical output signals representing the necessary flight parameters such as pressure altitude, mach number, airspeed, and impact pressure. See also COMPUTER, AIR SPEED; COMPUTER, ALTIMETER-PRESSURE; COMPUTER, ALTITUDE; COMPUTER, MACH NUMBER; COMPUTER, PRESSURE-ALTITUDE; COMPUTER, TRUE WIND DIRECTION AND INTENSITY; and COMPUTER, ZONE WIND. | RFQ |
Pitot Tube | 6610-01-503-2951 | A device used to measure the total pressure of a fluid stream. | RFQ |
Sensor,pressure | 6610-00-003-3957 | RFQ | |
Bottle,drain,aircraft Pitot Static | 6610-01-503-4379 | Container specifically designed for collection of moisture in aircraft pitot/static systems. Excludes SEPARATOR, PIPELINE and TRAP, MOISTURE. | RFQ |
Indicator,attitude | 6610-01-503-5060 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Indicator,attitude | 6610-01-503-5063 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Panel,flight Direct | 6610-01-503-5065 | RFQ | |
Computer,flight Director | 6610-01-503-5066 | An airborne analog computer used to combine signals from various navigational aids, gyroscopic controls, and landing systems in order to provide flight director steering signals to the pilot. Excludes COMPUTER, AIR NAVIGATION; COMPUTER, AZIMUTH; COMPUTER, COURSE-DISTANCE; COMPUTER, DESTINATION PRESET; and COMPUTER, HEADING. | RFQ |
Indicator,attitude | 6610-01-503-5068 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Indicator,attitude | 6610-01-503-5072 | An indicator which presents information showing the roll and pitch angles of an aircraft in relation to the earth. | RFQ |
Control-Display Unit | 6610-01-503-5407 | A component which performs the dual function of presenting visual information from other sources such as flight instruments and regulating the mode of operation of those sources. The item is essential for operation of the equipment. | RFQ |