ATTITUDE GYRO/2/ELECTRIC 4200-10Attitude Indicator | 2in, Rotating Roll, Traditional, 10-32VDCThe Model 4200 Electric Attitude Indicator incorporates a moving display that simulates the earth’s horizon and provides the pilot with a real time visual indication of the aircraft pitch and roll attitude relative to the indicator symbolic airplane.Version (Alternate Part# 4200-10) is a 2 inch 10-32VDC electric attitude indicator with rotating roll and traditional symbolic aircraft.Safe alternative to unreliable vacuum systemsSingle 4-pin connector installationIdeal standby artificial horizon in fixed-wing and helicopter applications10–32 volt DC operation for use in 14 and 28 volt aircraftStandard equipment on many OEM aircraftAnti-reflective glass enhances visibility and reduces fatigueLong-life LED lighting, user selectable to 5, 14 or 28 volt inputUse with optional MD420 or TS835 Emergency Power Supply to provide one hour or more of emergency attitude reference during an electrical failureCombine with a MD15 Altimeter and MD25 Airspeed Indicator for a complete standby package designed for tight panel applicationsFAA TSO-C4c certified and RTCA DO-160D/E qualifiedProduct CodesMfr Part No:4200-10ECCN:7A994PROAPP:PT3738CE, PQ3738CE, OL2R061LSCHEDULE B CODE:9014.20.6000TSO:C4cWeight: 1.6 lb Length: 5.94 in. MTBF: 2,500 Hours Power Input: 10–32 VDC: 14 VDC input (1.4A max start, 0.51A running) 28 VDC input (0.6A max start, 0.25A running) Dial: Rotating roll dial configuration, blue over brown Traditional symbolic airplane Panel Tilt: Aircraft specific — calibrated at factory Specify exact tilt between 0° and 20° when ordering Lighting: Internal LED lighting switchable to 5, 14 or 28 VDC input Wired through main connector Glass: Special HEA anti-reflective coating Mounting: Rear mount in standard 2" MS33638 panel cutout Temperature Range: –30°C to +70°C (–22°F to +158°F) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8-4S) Certification: FAA TSO-C4c RTCA DO-160D/E..

ATTITUDE GYRO/2/ELECTRIC 4200-11Attitude Indicator | 2in, Rotating Roll, Delta, 10-32VDCThe Model 4200 Electric Attitude Indicator incorporates a moving display that simulates the earth’s horizon and provides the pilot with a real time visual indication of the aircraft pitch and roll attitude relative to the indicator symbolic airplane.Version (Alternate Part# 4200-11) is a 2 inch 10-32VDC electric attitude indicator with rotating roll and delta symbolic aircraft.Safe alternative to unreliable vacuum systemsSingle 4-pin connector installationIdeal standby artificial horizon in fixed-wing and helicopter applications10–32 volt DC operation for use in 14 and 28 volt aircraftStandard equipment on many OEM aircraftAnti-reflective glass enhances visibility and reduces fatigueLong-life LED lighting, user selectable to 5, 14 or 28 volt inputUse with optional MD420 or TS835 Emergency Power Supply to provide one hour or more of emergency attitude reference during an electrical failureCombine with a MD15 Altimeter and MD25 Airspeed Indicator for a complete standby package designed for tight panel applicationsFAA TSO-C4c certified and RTCA DO-160D/E qualifiedProduct CodesMfr Part No:4200-11ECCN:7A994SCHEDULE B CODE:9014.20.8040TSO:C4cWeight: 1.6 lb Length: 5.94 in. MTBF: 2,500 Hours Power Input: 10–32 VDC: 14 VDC input (1.4A max start, 0.51A running) 28 VDC input (0.6A max start, 0.25A running) Dial: Rotating roll dial configuration, blue over brown Traditional symbolic airplane Panel Tilt: Aircraft specific — calibrated at factory Specify exact tilt between 0° and 20° when ordering Lighting: Internal LED lighting switchable to 5, 14 or 28 VDC input Wired through main connector Glass: Special HEA anti-reflective coating Mounting: Rear mount in standard 2" MS33638 panel cutout Temperature Range: –30°C to +70°C (–22°F to +158°F) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8-4S) Certification: FAA TSO-C4c RTCA DO-160D/E..

ATTITUDE INDICATOR/Electric, 10-32 VDC, Rotating Roll Dial, Delta Aircraft Symbol 4300-413Attitude Indicator | 3-1/8in, Electric, Rotating Roll, Delta, 10-32VDCThe Model 4300 Electric Attitude Indicator incorporates a moving display that simulates the earth’s horizon and provides the pilot with a real time visual indication of the aircraft pitch and roll attitude relative to the indicator symbolic airplane.Version (#AAP 4300-413) is a 3-1/8 inch 10-32VDC electric attitude indicator with rotating roll and delta symbolic aircraft.A safe alternative to unreliable vacuum systemsIdeal primary or standby artificial horizon in fixed-wing and helicopter applicationsSingle 4-pin connector installation7,500 hours MTBF — more than double the life of most electric gyros10–32 volt DC operation for use in both 14 and 28 volt aircraftField-replaceable lightingAnti-reflective glass enhances visibility and reduces pilot fatigueFAA TSO-C4c certified and RTCA DO-160D qualifiedDO-160 qualified for helicopter vibrationProduct CodesMfr Part No:4300-413SCHEDULE B CODE:9014.20.6000Weight: 2.7 lbs. Length: 6.6 inches MTBF: 7,500 Hours Certification: FAA TSO-C4c RTCA/DO-160D Power Input: 10–32 VDC: 1400 mA start, 600 mA max at 14 VDC input 700 mA start, 300 mA max at 28 VDC input Annunciators: STBY PWR (standby power mode) TEST (battery test — red/green) Lighting: 5, 14 or 28 VDC Incandescent Field-replaceable tray wired through main connector Glass: Special HEA anti-reflective coating Mounting: Rear mount in standard 3 1/8” round panel cutout Temperature Range: –30°C to +70°C (–22°F to +158°F) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8–4S) Panel Tilt: Aircraft specific — calibrated at factory Specify exact tilt between 0° to 20° when ordering Dial: Rotating roll dial, traditional symbolic airplane..

ATTITUDE INDICATOR/Electric, 10-32 VDC, Rotating Roll Dial, Traditional Symbolic Aircraft. 4300-411/0ATTITUDE INDICATOR/Electric, 10-32 VDC, Rotating Roll Dial, Traditional Symbolic Aircraft. Fly with confidence and peace of mind. Fly with Mid-Continent Instruments' new 4300 series electric attitude indicator the Lifesaver gyro. Even if every other system in your aircraft's avionics panel goes dark, the Lifesaver powers on. The only attitude indicator with a self-contained battery backup, it delivers one full hour of emergency attitude reference. One hour of precious time to pull you through when trouble strikes and all other power fails. Can you live without it? Features: Custom versions available to match existing instrument/EFIS displaysOptional self-contained battery backup features built-in annunciators and internal emergency lightingUp to one hour of emergency attitude referenceEasy to install with single connector for primary and optional standby battery modelsExceptional value with 7,500 hours MTBF, more than double the life of most electric gyrosDesigned as the primary or standby artificial horizon in fixed and rotor-wing aircraft.May be installed in place of an existing turn coordinator or turn and slip indicator per FAA advisory circular AC91-75, or as a replacement for the existing attitude gyro per advisory circular AC20-41A.10-32 volt DC replacement for use in either 14 or 28 volt aircraftAnti-reflective glass enhances visibility and reduces fatigueField replaceable lightingApproved to FAA TSO-C4c, RTCA DO160DOne-year manufacturer's limited warranty Product CodesMfr Part No:4300-411/0ECCN:7A994SCHEDULE B CODE:9014.20.6000TSO:C4c..

ATTITUDE INDICATOR/Electric, 10-32VDC, 10 Degree Tilt, 28V Lighting 4300-411Attitude Indicator | 3-1/8in, Electric, Rotating Roll, Traditional, 10-32VDC, 10º Tilt, 28V LightingThe Model 4300 Electric Attitude Indicator incorporates a moving display that simulates the earth’s horizon and provides the pilot with a real time visual indication of the aircraft pitch and roll attitude relative to the indicator symbolic airplane.Version (#AAP 4300-41110) is a 3-1/8 inch 10-32VDC electric attitude indicator with rotating roll, traditional symbolic aircraft, 11º tilt, and 28V lighting.A safe alternative to unreliable vacuum systemsIdeal primary or standby artificial horizon in fixed-wing and helicopter applicationsSingle 4-pin connector installation7,500 hours MTBF — more than double the life of most electric gyros10–32 volt DC operation for use in both 14 and 28 volt aircraftField-replaceable lightingAnti-reflective glass enhances visibility and reduces pilot fatigueFAA TSO-C4c certified and RTCA DO-160D qualifiedDO-160 qualified for helicopter vibrationProduct CodesMfr Part No:4300-411ECCN:7a994SCHEDULE B CODE:9014.20.6000TSO:C4cWeight: 2.7 lbs. Length: 6.6 inches MTBF: 7,500 Hours Certification: FAA TSO-C4c RTCA/DO-160D Power Input: 10–32 VDC: 1400 mA start, 600 mA max at 14 VDC input 700 mA start, 300 mA max at 28 VDC input Annunciators: STBY PWR (standby power mode) TEST (battery test — red/green) Lighting: 5, 14 or 28 VDC Incandescent Field-replaceable tray wired through main connector Glass: Special HEA anti-reflective coating Mounting: Rear mount in standard 3 1/8” round panel cutout Temperature Range: –30°C to +70°C (–22°F to +158°F) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8–4S) Panel Tilt: Aircraft specific — calibrated at factory Specify exact tilt between 0° to 20° when ordering Dial: Rotating roll dial, traditional symbolic airplane..

ATTITUDE INDICATOR/Electric, Rotating roll dial, Traditional symbolic aircraft, 10-32 VDC. 4300-311Attitude Indicator | 3-1/8in, Electric, Rotating Roll, Traditional, 10-32VDC, 11º TiltThe Model 4300 Electric Attitude Indicator incorporates a moving display that simulates the earth’s horizon and provides the pilot with a real time visual indication of the aircraft pitch and roll attitude relative to the indicator symbolic airplane.Version (#AAP 4300-31111) is a 3-1/8 inch 10-32VDC electric attitude indicator with rotating roll, traditional symbolic aircraft, and 11º tilt.A safe alternative to unreliable vacuum systemsIdeal primary or standby artificial horizon in fixed-wing and helicopter applicationsSingle 4-pin connector installation7,500 hours MTBF — more than double the life of most electric gyros10–32 volt DC operation for use in both 14 and 28 volt aircraftField-replaceable lightingAnti-reflective glass enhances visibility and reduces pilot fatigueFAA TSO-C4c certified and RTCA DO-160D qualifiedDO-160 qualified for helicopter vibrationProduct CodesMfr Part No:4300-311TSO:C4cWeight: 2.7 lbs. Length: 6.6 inches MTBF: 7,500 Hours Certification: FAA TSO-C4c RTCA/DO-160D Power Input: 10–32 VDC: 1400 mA start, 600 mA max at 14 VDC input 700 mA start, 300 mA max at 28 VDC input Annunciators: STBY PWR (standby power mode) TEST (battery test — red/green) Lighting: 5, 14 or 28 VDC Incandescent Field-replaceable tray wired through main connector Glass: Special HEA anti-reflective coating Mounting: Rear mount in standard 3 1/8” round panel cutout Temperature Range: –30°C to +70°C (–22°F to +158°F) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8–4S) Panel Tilt: Aircraft specific — calibrated at factory Specify exact tilt between 0° to 20° when ordering Dial: Rotating roll dial, traditional symbolic airplane..

CARBURETOR TEMPERATURE PROBE B-5 PROBECARBURETOR TEMPERATURE PROBE Mid-Continent Instrument's B-5 Probe is the only FAA Approved S.T.C.'d internal carburetor temperature sensing device. Designed for use with all Marvel-Schebler and Bendix Float-Type carburetors, the B-5 is the only probe that installs at the throttle valve - the critical icing point in fuel induction systems. Used with the MD-11 Gauge, pilots can monitor and control carburetor heating to within 1C for maximum safety and engine efficiency. Eliminate carburetor icing Reduce spark plug fouling Extend engine life Increase range and power Gain maximum fuel economy The B-5 probe is THE ONLY FAA PMA certified carburetor ice probe available!Product CodesMfr Part No:B-5 PROBEECCN:9A991PMA:PQ3738CESCHEDULE B CODE:9025.90.0000STC:SE1-201..

DIRECTIONAL GYRO/Electric, 10-32 VDC, 28V lighting. 3300-11Directional Gyro | 10-32VDC, 28V LightingThe Model 3300 Directional Gyro (DG) is a gyroscopic directional indicator. This short-term directional reference is used in conjunction with a magnetic compass. The directional gyro excels in providing a direction indication during maneuvers when the magnetic compass develops errors.Weighs just 1.9 lbs. – One pound less than most electric directional gyrosMulti-voltage 10–32 volt DC input remains valid until the aircraft main battery discharges to 10 VDCDirect replacement for many AIM205 and RC Allen RCA15 unitsDesigned specifically for use in high vibration applicationsWarning flag monitors rotor speed and power inputAnti-reflective glass enhances visibility and reduces fatigueWorldwide support programRequires less than half the power of standard directional gyrosLong-life LED lighting, user selectable to 5, 14 or 28 volt input with adjustable brightnessFAA TSO-C5e certified and RTCA DO-160E qualifiedExceptional RTCA DO-160E HIRF immunityProduct CodesMfr Part No:3300-11ECCN:7A994SCHEDULE B CODE:9014.10.7040TSO:C5eWeight: 1.9 lbs. Length: 4.65 in. Power Input: 10–32 VDC Current Rating: At 14 VDC, Start: 1.4A Max., Run: 0.44A nominal At 28 VDC, Start: 0.6A Max., Run: 0.22A nominal Lighting: Internal LED lighting 28 VDC input Adjustable brightness MTBF: 2,500 hours Temperature Range: –40°C to +55°C (–40°F to 130°F) Altitude: –15,000 to +50,000 feet Connector: 4-pin (MS3116E8-4P) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8-4S or equivalent) Color: Index Marks, Text, Symbolic Airplane, Logo: White Bezel, Dial Background: Black Power/Rotor Speed Warning Flag: Red Glass: Special HEA anti-reflective coating Mounting: Rear panel mount in standard 3 1/8” round panel cutout..

DIRECTIONAL GYRO/Electric, 10-32 VDC. 3300-10Directional Gyro | 10-32VDCThe Model 3300 Directional Gyro (DG) is a gyroscopic directional indicator. This short-term directional reference is used in conjunction with a magnetic compass. The directional gyro excels in providing a direction indication during maneuvers when the magnetic compass develops errors.Weighs just 1.9 lbs. – One pound less than most electric directional gyrosMulti-voltage 10–32 volt DC input remains valid until the aircraft main battery discharges to 10 VDCDirect replacement for many AIM205 and RC Allen RCA15 unitsDesigned specifically for use in high vibration applicationsWarning flag monitors rotor speed and power inputAnti-reflective glass enhances visibility and reduces fatigueWorldwide support programRequires less than half the power of standard directional gyrosFAA TSO-C5e certified and RTCA DO-160E qualifiedExceptional RTCA DO-160E HIRF immunityProduct CodesMfr Part No:3300-10ECCN:7a994SCHEDULE B CODE:9014.10.7040TSO:C5eWeight: 1.9 lbs. Length: 4.65 in. Power Input: 10–32 VDC Current Rating: At 14 VDC, Start: 1.4A Max., Run: 0.44A nominal At 28 VDC, Start: 0.6A Max., Run: 0.22A nominal MTBF: 2,500 hours Temperature Range: –40°C to +55°C (–40°F to 130°F) Altitude: –15,000 to +50,000 feet Connector: 4-pin (MS3116E8-4P) Mating Connector: Mid-Continent P/N 9015514 (MS3116F8-4S or equivalent) Color: Index Marks, Text, Symbolic Airplane, Logo: White Bezel, Dial Background: Black Power/Rotor Speed Warning Flag: Red Glass: Special HEA anti-reflective coating Mounting: Rear panel mount in standard 3 1/8” round panel cutout..

Electric Attitude indicator, 2 inch TSO, Mid-Continent 4200 Series MDCT 4200-10..

Electric Attitude indicator, 2 inch TSO, Mid-Continent 4200 Series MDCT 4200-11..

HTAWS (Helicopter Terrain Awareness Warning System) ANNUNCIATION CONTROL UNIT/28V, Horizontal. For use with Honeywell Mark XXI. MD41-1368MD41 Series Helicopter TAWS Annunciation Control Unit | 28V, Horizontal, Mark XXI EGPWSThe MD41 Helicopter TAWS Annunciation Control Unit is a three-button horizontal 28 volt TAWS for Honeywell Mark XXI EGPWS. Designed to place annunciation and mode selection for the Terrain Awareness Warning System (TAWS) within the pilots direct field-of-view, these annunciators provide tactile feedback to the pilot through internally-lighted push buttons.Version (Alternate Part# MD41-1368) is a 28V unit with horizontal orientation for helicopter applications. Compatible with Honeywell Mark XXI EGPWS.Control unit provides annunciation and mode selection for HTAWS (Helicopter Terrain Awareness Warning System)Presents primary or secondary visual alert of HTAWS within the pilot’s direct field of viewReduced installation costs:Single cutoutPanel punches availableEasy-to-wire D-subminiature connectorProven daylight-readable annunciations with automatic photocell dimmingInternally lighted push-buttons provide firm tactile feedback to the pilotRemote annunciator test capabilityCertified to TSO C151aMeets RTCA DO-160D environmental specifications (certified to 55,000 feet)Quality Mil-Spec connector includedProduct CodesMfr Part No:MD41-1368ECCN:9A991SCHEDULE B CODE:8536.50.9030TSO:C151aWeight: 0.50 lbs. Dimensions: 0.80”H x 3.25”W x 3.20”D (not including connector or mate) Orientation: Horizontal Power Input: 28 VDC Lighting Input: 28 VDC Mating Connector: Positronic RD25F10JVL0 or equivalent (Mid-Continent P/N 7014517) Instrument Panel Mounting: Rear mount Qualification: FAA TSO-C151 Environmental Qualification: RTCA DO-160D Power Requirement: 0.15 A max..

MD302 SAM STANDBY ATTITUDE MODULE 6420302-1MD302 Standby Altitude Module | Black Bezel, Li-ion BatteryThe MD302 Standby Altitude Module or SAMâ„¢ features a unique two-screen display that provides attitude, altitude, airspeed, slip, vertical trend, and heading information to the pilot during normal or standby operation in the event of primary instrument failure. This self-contained, solid-state instrument features a selectable orientation, horizontal or vertical, which allows flexible cockpit design and installation. The MD302 is also equipped with a rechargeable Nanophosphate® lithium-ion battery that provides up to one hour of emergency operation when fully charged.This MD302 Standby Altitude Module (Alternate Part# MD302-1): Black bezelLi-ion BatteryFeatures: Attitude, altitude, airspeed, slip, and vertical trend indicationOptional Heading via the MD32 Magnetometer or aircraft systemFive primary functions utilize modern solid-state MEMS gyro, accelerometer and pressure transducer technologyCompact footprint — only 2.4 x 5.5 inchLightweight — Only 1.6 lbSelf-contained, rechargeable, field-replaceable emergency batterySmooth, high-definition graphicsUnique two-screen display with wide viewing angles and a user-friendly menu structure Selectable horizontal and vertical orientationsAircraft-specific, programmable airspeed range markingsConfigurable for static source error correction (SSEC)Simple user interface — one knob configures the display and provides menu controlExternal, automatic and manual dimming control settingsSoftware configurable lighting curvesField-upgradable software via standard USB portDesigned and built in Wichita, Kansas, USAProduct CodesMfr Part No:6420302-1ECCN:7a994PROAPP:PT3738CE, PQ3738CE,OL2R061LSCHEDULE B CODE:9014206000SIN:334511TSO:C2d(Type B), C3e, C4c, C6e, C10b, C106, C113a, C179a Hazmat charges may applyWeight: 1.6 lb (0.73 kg) Dimensions: 5.50 x 2.37 x 5.17 in Power Input: 10 VDC — 32 VDC, 6 watt (nominal), 40 watt (maximum) Output: ARINC 429 (high or low speed, see manual for specific labels) Operating Range: Attitude: 300° per second pitch, roll and yaw (max) Altitude; -1,500 to 55,000 ft (-457 to 16,764 m) Airspeed: 20 to 500 knots (23 to 575 mph) (37 to 926 kph) Vertical Trend: 6 second time frame Heading: Within ±2° up to 55°N or 45°S Units of Measure: Altitude: Feet or meters Barometric Setting: Inches of mercury, millibars Airspeed: Knots, miles per hour or kilometers per hour Panel Tilt: -90° to +90° pitch, configurable Panel Roll: -5° to +5° roll, configurable Lighting: 5 VDC, 14 VDC, and 28 VDC external input or internal photocell Programmable dimming curve Pilot Interface: 16-detent, push and turn knob Battery: Rechargeable, field-replaceable, internal battery Technology: Nanophosphate® lithium-ion or nickel metal hydride Run Time: 60 minutes minimum when fully charged and properly maintained Mounting: Front Panel Mount Mating Connectors: Mid-Continent P/N 9017646 kit contains custom DB15 connector with configuration module, pitot and static connectors Certification: FAA TSO certified C2d, C3e, C4c, C6e (incomplete), C10b, C106, C113a, C179a  ANAC TSO certified C2d, C3e, C4c, C10b, C106, C113a, C179a  EASA ETSO certified C2d, C3d (incomplete), C4c, C10b, C106, C113, C179a  RTCA DO-178B and DO-254 Design Assurance Level (DAL) A RTCA DO-160 and RTCA DO-311 qualified..

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