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Electronics International 2 Inter Turbine Temperature Gauge Tr-1-Itt-P Prem Package
MFR Model# TR-ITT-P
Overview
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The TR-1-ITT (Inter Turbine Temperature) instrument is configured to interface with a Type-K thermocouple probe. The TR-1-ITT incorporates a map which is used to compensate for nonlinearities in the voltage vs temperature curves of the probe. This instrument has exceptional performance, reliability and features; a design driven by the 38+ years of experience. The TR-1-ITT Instrument was designed as a replacement for existing 2″ ITT instruments. Depending on your current installation you may need to wire in aircraft power and ground. The instrument features a 210° analog arc, backlight and a dimmable, digital display. The instrument’s faceplate will be custom built to match your aircraft’s limits (red/yellow markings). The TR-1-ITT fits into a 2″ standard round hole (MS28041-1A mount) and is 4.23″ long. It is FAA Certified to TSO: -C43c, -C44c, -C45b, -C47a, -49b, -C55a and comes with an FAA 8130-3 Airworthiness Approval Tag.
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Features
TR-1-NP RPM (Standard Pkg)- 1 Year Warranty
- FAA TSO’d
- No Risk 3-Month Money-Back Guarantee
- 8130-3 Airworthiness Approval Tag Provided
- 3 Year Warranty
- FAA TSO’d
- No Risk 3-Month Money-Back Guarantee
- 8130-3 Airworthiness Approval Tag Provided
- 1000+ hours of recording at 1 second per record.
- Priority service on warranties and orders.
- Free overnight shipping on warranties and orders.
- Warranties handled by providing an exchange unit.
- Custom-printed faceplates with your aircraft’s markings will be held in stock.
- Replacement units will be held in stock.
- Exchange the TR-1-TQ for an MVP-50T within one year and get full credit on your returned TR-1-TQ towards the purchase price of an MVP-50T.
Specifications
- Size: 1.932″ Dia, 4.23″ long (Not including the connector), 2.0″ dia Bezel
- Mount: MS28041-1A, Two Inch Round
- Weight: 0.3 Lbs.
- Environmental: Designed and Tested to TSO, DO-160G
- Software: Designed and Documented to DO-178C, Level C
- Minimum Performance Standards: TSO‐C43c, TSO‐C44c, TSO‐C45b, TSO‐C47a, TSO‐49b, and TSO‐C55a.
- Power Requirements: 6.0 to 55 Volts, 0.075 Amps @ 28V (Typ), 0.05 Amps @ 14 Volts (Typ).
- Communication Port: RS232
- Display Area: Backlit for night operation. Optional Red and/or Yellow Warning Lights
- Dimming Circuits: Electric eye and Control Voltage Input. * Analog Pointer: 210° sweep, Backlit.
- Digital Display: 4 digits, -999 to 9999 (or -99.9 to 999.9) readings, Dimmable.
- Data Recording: 1000 Hours at 1 second per record, accessible via RS232 Port.
Q&A
Please note, Aircraft Spruce Australia's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce Australia assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
PER EI: "While the TR-1-ITT would work well as a replacement for the M-1-ITT, it is not quite a plug and play installation. Some rewiring would need to be performed, and an adapter plate (A-104) would be required to fit the TR-1-ITT in the M-1-ITT's 2-1/4" hole."
