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MS28034-3 Engine Temperature Sensor
MFR Model# MS28034-3
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Overview
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Presently in use in government and general aviation industry under liquid and gaseous conditions, this sensing device exceeds stringent U.S. Military Specifications for response time, burst pressure, and AC high potential tests. |
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WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov. |
Features
- Fast Response
- Single Element
- Hermetic Seal, Tip
- Weld Internal Construction
- Low Stem Conduction
- Integral Connector
- 2-Wire Element
- Corrosion Resistant
- Thread Mounted
Specifications
- Response Time: (63.2% of Step) 1.3 sec. (typ.)
- Insulation Resistance: 1000 Megohms @ 100 VDC
- AC Breakdown: <.5 ma @ 500 VAC
- Operating Pressure: 200 PSI
- Burst Pressure: >600 PSI
- R vs. T Curve Data: Per MIL-T-7990B, Table I
- Self-Heating: Error
- Operating Temp. Range: -70° C to 300°C
- Vibration Specification: MIL-STD-810C, Method 514.2 Procedure I, Cat. B.I, Curve L
- Weight: .12 lbs (Typ.)
- MIL or Standards Society Spec: MIL-T-7990B, MIL-STD-810, MIL-C-5015, MS28034, FED-STD-151, MIL-STD-105
- Materials: Stainless steel housing and connector shell with
- FAS-TIP sensing element
Q&A
Please note, Aircraft Spruce'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 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.
