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1. Barometric Altimeter
 BG-3E
BG-3H
BG10-2
BG3
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Model: BG-3 SERIES
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Application: It is used to measure the relative altitude of an aircraft in flight.
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Measuring Range: -1000~20,000ft
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Operation Temperature: -30~+50℃
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Indication accuracy: conforms to As 392c
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Dimension: 82.5 x 105
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Weight: <700g
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BG-3
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28.1~31.0 inHg, -1000~20,000ft
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3-pointer, ten thousand pointer in plate form 3 1/8"
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2
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BG-3A
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950~1,050Mbar, -1000~20,000ft
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3-pointer, ten thousand pointer in plate form 3 1/8"
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3
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BG-3B
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28.1~31.0 inHg, -1000~20,000ft
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3-pointer, 3 1/8"
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4
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BG-3E
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950~1,050Mbar, -1000~20,000ft
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3-pointer, 3 1/8"
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5
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BG-3H
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-1000~20,000ft, 950~1,050Mbar, 28.1~31.0 inHg
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Two baro-windows, 3-pointer, 3 1/8"
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Model: BG-7 SERIES
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Application: It is used to indicate the relative altitude of an aircraft, fitting for sports gliders.
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Measuring Range: 0~5,500ft
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Max Measurement: 12,000ft
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Barometric Scale Range: 28~31 inHg
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Operation Temperature: -20~+50℃
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Dimension: 82.5 x 82.5 x 73
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Weight: <350g
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Specifications: single pointer
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BG-7
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0~5,500ft, 28~31 inHg
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3 1/8"
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2
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BG-12A
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0~5,500ft, 50~1,050Mbar
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3 1/8"
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Model: BG-11 SERIES
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Application: It is used to indicate the relative altitude of an aircraft, fitting for sports gliders.
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Measuring Range: 0~10,000ft
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Barometric Scale Range: 28~31 inHg
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Operation Temperature: -20~+50℃
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Dimension: 82.5 x 82.5 x 73
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Weight: <350g
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BG-11
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0~10,000ft, 28~31 inHg
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3 1/8"
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2
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BG-11A
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0~10,000ft, 950~1,050Mbar
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3 1/8"
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3
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BG-11B
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0~300m, 950~1,050Mbar
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3 1/8"
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Model: Single-Pointer Altimeter
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Application: It is used to indicate the relative altitude of an aircraft in the flight.
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Operation Temperature: -30~+50℃
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Dimension: 60 x 60 x 109
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Weight: <120g
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BG-9
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0~5,000ft, 27~31 inHg
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2 1/4"cut out (Φ57x78.5)
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2
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BG-10
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0~10,000ft, 27~31 inHg
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2 1/4"cut out (Φ57x78.5)
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3
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BG-15
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0~10,000ft, 27~31 inHg
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2 1/4"cut out (Φ57x78.5)
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4
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BG3
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0~3,000m, 910~1,050Mbar
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2 1/4"cut out (Φ57x78.5)
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5
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BG6-1A
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0~6,000m, 900~1,050Mbar
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2 1/4"cut out (Φ57x78.5)
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6
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BG6-2
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0~6,000m, 700~1,040Mbar
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3 1/8"cut out (Φ80x52.6)
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7
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BG-14
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0~6,000m, 900~1,050Mbar
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2 1/4"cut out
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8
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BG10-2
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0~10,000m, 600~1,040Mba
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3 1/8"cut out (Φ80x52.5)
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2. Accelerometer ("G" Meter)
BJ10-2F
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BJ10-2F
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-5~+10g
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2 1/4"cut out
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3. Manifold Pressure Indicator
BYJ-3
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BYJ-3
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10~50 inHg
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3 1/8"cut out
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4. Oil Temperature and Pressure Indicator
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BWY-8
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0~100Ib/in, 40~28℉, 4.4~137.88℃
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3 1/8"cut out
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5. Airspeed indicator
BK150-1A
BK-240
BK-7B
BK300
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Application: It is used to measure the indicated airspeed of an aircraft.
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Operation Temperature: -20~+50℃
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Indicating Accurace: conforming to AS8019
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Weight: <350g
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BK-3
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20-160mph, 20-140 knots
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3 1/8''Cut out (Φ79.4 x 97.3)
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2
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BK-3A
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20-140 knots
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3 1/8''Cut out (Φ79.4 x 97.3)
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3
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BK-4
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30-180mph, 30-160 knots
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3 1/8''Cut out (Φ79.4 x 97.3)
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4
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BK-5
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30-250mph,30-220 knots
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3 1/8''Cut out (Φ79.4 x 97.3)
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5
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BK-5A
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30-220knot
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3 1/8''Cut out (Φ79.4 x 97.3)
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6
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BK-10
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30-200mph, 30-180knots
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3 1/8''Cut out (Φ79.4 x 97.3)
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7
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BK-11
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30-200mph, 30-170knots
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3 1/8" (Φ80 x 58) out.:mph, inside.:knots
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8
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BK-11A
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30-200mph, 30-170knots
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3 1/8" (Φ80 x 58) out.:knots, inside.:mph
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9
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BK-9C
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20-8 mph
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3 1/8" (Φ80 x 58) Dense scale
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10
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BK-8D
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20-100mph
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3 1/8" (Φ80 x 58) Dense scale
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11
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BK-7B
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20-120mph
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3 1/8" (Φ80 x 58) Dense scale
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12
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BK-6C
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20-150mph
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3 1/8" (Φ80 x 58) Dense scale
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13
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BK-12
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20-80knots
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3 1/8" (Φ80 x 58)
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14
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BK-13A
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20-100knots
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3 1/8" (Φ80 x 58) Dense scale
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15
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BK-14A
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20-120knots
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3 1/8" (Φ80 x 58) Dense scale
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16
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BK-40
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20-250knots
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3 1/8" (Φ80 x 58)
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17
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BK-15
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20-160knots
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3 1/8" (Φ79.4 x 97.3)
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18
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BK-25
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40-260knots
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3 1/8" (Φ79.4 x 97.3)
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19
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BK120-1B
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30-120kph
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3 1/8" (Φ80 x 58)
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20
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BK150-1A
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30-150kph
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3 1/8" (Φ80 x 58)
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21
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BK200-1A
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30-200kph
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3 1/8" (Φ80 x 58)
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22
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BK240
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30-240kph
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3 1/8" (Φ80 x 58)
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23
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BK300
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30-300kph
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3 1/8" (Φ80 x 58)
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24
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BK-31
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20-140mph
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3 1/8" (Φ80 x 97)
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25
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BK-32
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20-160mph
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3 1/8" (Φ80 x 97)
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26
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BK-33
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30-180mph
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3 1/8" (Φ80 x 97)
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27
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BK-34
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30-180mph
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3 1/8" (Φ80 x 97)
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28
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BK-35
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30-200mph
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3 1/8" (Φ80 x 97)
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29
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BK-36
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20-80mph
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2 1/4" cut out (Φ57 x 60) with 0 scale
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30
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BK-37
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20-100mph
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2 1/4" cut out (Φ57 x 60) with 0 scale
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31
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BK-38
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20-120mph
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2 1/4" cut out (Φ57 x 60) with 0 scale
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32
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BK-20
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20-80mph
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2 1/4" cut out (Φ57 x 60) no 0 scale
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33
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BK-21
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20-100mph
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2 1/4" cut out (Φ57 x 60) no 0 scale
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34
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BK-22
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20-120mph
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2 1/4" cut out (Φ57 x 60) no 0 scale
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35
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BK-23
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20-140mph
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2 1/4" cut out (Φ57 x 60) no 0 scale
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36
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BK-42
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20-140mph
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2 1/4" cut out (Φ57 x 60) with 0 scale
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6. Vertical Speed Indicator
BC-2A
BC10-1B
BC-6A
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Application: It is used to indicate the vertical speed of an aircraft.
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Operation Temperature: -20~+50℃
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Indicating Accurace: conforming to TSO-C8C (AS8016)
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Weight: <500g
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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BC-3
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0~+/-3,000 ft/min
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Figure outside, scale inside,
3 1/8"cut out
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2
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BC-4
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0~+/-4,000 ft/min
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Figure outside, scale inside,
3 1/8"cut out
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3
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BC-2A
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0~+/-2,000 ft/min
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Figure outside, scale inside,
3 1/8" inside, 3 1/8"cut out
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4
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BC-6
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0~+/-2,000 ft/min
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Figure outside, scale inside,
2 1/4" cut out outside,
2 1/4"cut out
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5
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BC-6A
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0~+/-10 m/s
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2 1/4''Cut out
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6
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BC-10-1B
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0~+/-10 m/s
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3 1/8''Cut out
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7. Engine Instruments
EGT/EGT
EGT PROBES
CHT/CHT2
CHT PROBES
WATER TEMP. GAUGE
VOLTMETER
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Model: EGT SERIES
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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L9114
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600-1,700°F/100-1000°C
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EGT 2" FAHR./CEL
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2
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L9218
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600-1,700°F
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EGT 2" FAHR.
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3
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L9219
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100-1000°C
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EGT 2'' CEL.
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4
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L917
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600-1700°F/100-1000°C
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EGT 2 1/4'' FAHR./CEL.
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5
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L928
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600-1700°F
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EGT 2 1/4'' FAHR.
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6
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L929
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100-1000°C
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EGT 2 1/4'' CEL
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7
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L205C
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600-1700°F
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EGT 3 1/8'' FAHR.
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8
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L9126
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600-1700°F
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EGT/EGT 2'' FAHR
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9
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L9214
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100-1000°C
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EGT/EGT 2'' CEL.
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10
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L9127
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600-1700°F
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EGT/EGT 2 1/4'' FAHR.
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11
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L9215
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100-1000°C
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EGT/EGT 2 1/4'' CEL.
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12
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L207C
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600-1705°F
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EGT/EGT 3 1/8'' FAHR.
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13
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L912A
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M 8X1 SCREW TYPE
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EGT PROBES
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14
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L912B
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Z 1/8 SCREW TYPE
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EGT PROBES
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Model: CHT SERIES
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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L918
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0-700°F/0-350°C
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CHT 2'' FAHR./CEL.
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2
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L926
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0-700°F
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CHT 2'' FAHR.
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3
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L927
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0-350°C
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CHT 2'' CEL.
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4
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L9125
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0-700°F/0-350°C
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CHT 2 1/4'' FAHR./CEL.
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5
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L9216
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0-700°F
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CHT 2 1/4'' FAHR.
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6
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L92177
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0-350°C
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CHT 2 1/4'' CEL.
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7
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L206C
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0-700°F
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CHT 3 1/8'' FAHR.
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8
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L9124
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0-700°F
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CHT/CHT 2'' FAHR.
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9
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L9213
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0-350°C
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CHT/CHT 2'' CEL.
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10
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L9123
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0-700°F
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CHT/CHT 2 1/4'' FAHR.
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11
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L9212
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0-350°C
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CHT/CHT 2 1/4'' CEL
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12
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L208C
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0-700°F
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CHT/CHT 3 1/8'' FAHR.
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13
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L913C
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14MM METAL SLEEVE
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CHT PROBES
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14
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L913E
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10MM METAL SLEEVE
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CHT PROBES
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15
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L913D
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12MM METAL SLEEVE
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CHT PROBES
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16
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L913B
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18MM METAL SLEEVE
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CHT PROBES
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Model: WATER TEMP. GAUGE SERIES
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
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DESCRIPTION
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1
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L9128A
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100-250°F/40-120°C
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2'' FAHR./CEL.
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2
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L9128
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100-250°F/40-120°C
|
2 1/4'' FAHR.
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3
|
L210C
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100-250°F/40-120°C
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3 1/8'' CEL.
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Model: VOLTMETER SERIES
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SPECIFICATIONS
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SERIAL NO.
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MODEL NO.
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MEASURING RANGE
|
DESCRIPTION
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1
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L211A
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6-16V
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2''
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2
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L211B
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6-16V
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2 1/4''
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3
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L211C
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6-16V
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3 1/8''
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8. Compass
CM-13
CM-24
MC-022
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Model: CM-13, CM-13L MAGNETIC COMPASS (LIQUID COMPASS)
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Features:It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation. CM-13L has a lighting system (12V, 24V & 36V).
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Specifications:
1. Error of the comapss is no more than 2.5 degree.
2. Friction error is no more than 1 degree.
3. When an aircraft tilts for 10, the error is no more than 4 degree.
4. Ambient temperature is -55 to +60 ℃
5. It is in accordance with the standard of TSO-C7d.
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SPECIFICATIONS
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SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
CM-13
|
|
|
|
Model: CM-24
|
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Features: It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation. CM-24L has a lighting system (12V, 24V & 36V)
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Specifications: When the compass compensation is adjusted to neutral position, the error of the compass is ±2.5 degree. Fiction error is no more than 1 degree. The effect of the compass compensation is from 10 to 40 degree. Ambient temperature is -60 to +60 degree centigrade.
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Antivibration: It is in accordance with the technical specifications. When the compass is in the ambient condition of 20-50HZ frequency, 1.5g overload vibration; when there is 3h vibration, it has not any kind of mechanical damage. It is in accordance with the standard of TSO-C7d.
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SPECIFICATIONS
|
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SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
CM-24
|
|
CM024L MAGNETIC COMPASS ( LIQUID COMPASS )
|
|
Model: MC MAGNETIC COMPASS (VERTICAL CARD AND NON-LIQUID)
|
|
Features: MC022 magnetic compass can provide directional reference of geomagnetic meridian and indicate magnetic heading of an aircraft. It has advantages of simple structure, good independence and reliable operation. It is an indispensable compass in aviation. It is mainly used in small aircraft, indicating magnetic heading.
|
|
Specifications:
1. 360 degree azimuth can be seen clearly by adopting vertical azimuth dial.
2. Scale error is no more than 4 degree.
3. Compensation range of compass corrector is 15 to 40 degree.
4. It is in accordance with the standard of TSO-C7d.
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|
SPECIFICATIONS
|
|
SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
MC-022
|
|
|
|
|
9. Turn Co-ordinator
BZW-4B
|
|
Model: BZW-4B TURN CO-ORDINATOR
|
|
Features:
· Object display and mark
· Precision electrical gyroscope
· Small in size, light in weight
· Simple construction, convenience in maintenance
· Power failure warning
|
|
Specifications:
· Voltage: 12 to 32 V DC
· Electrical consumption: starting current(no more than 1.5A),operating current (no more than 0.35A)
· Operating range: 2 min. Turn
· Weight: 0.47Kg (16.55ozs )
|
|
Model: BZW-4D TURN CO-ORDINATOR LIGHTED
|
|
Features:
· Object display and mark
· Precision electrical gyroscope
· Small in size, light in weight
· Simple construction, convenience in maintenance
· Power failure warning
|
|
Specifications:
· Voltage: 12 to 32 V DC
· Electrical consumption: starting current(no more than 1.5A),operating current (no more than 0.35A)
· Operating range: 2 min. Turn
· Weight: 0.47Kg (16.55ozs )
|
|
|
10. Directional GYRO-Electric
GD023
|
|
Model: GD023 DIRECTIONAL GYRO-ELECTRIC
|
|
Function: Indicating heading of an aircraft.
|
|
Specifications:
|
|
Operation Voltage: DC. 14±1% V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20±5 ℃
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1. Working Range: Indicating heading angle within the range of 360°
2. Accuracy: The drift error is not more than 4°/10min.
3. It will work normally when operation voltage is inputted 3min.and rotor starts working when 80% operating voltage is inputted.
4. Operating current is not more than 0.72A.
5. Rated rotating speed is 22000 turns per min; It warns when power-off the rotating speed is below 70% of the rate rotating speed.
6. The insulating resistance between the power and case is not less than 20 MΩ.
7. It is in accordance with the standard of TSO-C4c.
|
|
Model: GD023L DIRECTIONAL GYRO-ELECTRIC WITH 14V LIGHTED
|
|
Function: Indicating heading of an aircraft.
|
|
Specifications:
|
|
Operation Voltage: DC. 14±1% V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20±5 ℃
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1. Working Range: Indicating heading angle within the range of 360°
2. Accuracy: The drift error is not more than 4°/10min.
3. It will work normally when operation voltage is inputted 3min.and rotor starts working when 80% operating voltage is inputted.
4. Operating current is not more than 0.72A.
5. Rated rotating speed is 22000 turns per min; It warns when power-off the rotating speed is below 70% of the rate rotating speed.
6. The insulating resistance between the power and case is not less than 20 MΩ.
7. It is in accordance with the standard of TSO-C4c.
|
|
Model: GD023BL DIRECTIONAL GYRO-ELECTRIC WITH 28V LIGHTED
|
|
Function: Indicating heading of an aircraft.
|
|
Specifications:
|
|
Operation Voltage: DC. 28 ±1%V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20±5 ℃
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1. Working Range: Indicating heading angle within the range of 360°
2. Accuracy: The drift error is not more than 4°/10min.
3. It will work normally when operation voltage is inputted 3min.and rotor starts working when 80% operating voltage is inputted.
4. Operating current is not more than 0.72A.
5. Rated rotating speed is 22000 turns per min; It warns when power-off the rotating speed is below 70% of the rate rotating speed.
6. The insulating resistance between the power and case is not less than 20 MΩ.
7. It is in accordance with the standard of TSO-C4c.
|
|
|
11. Horizon GYRO- Electric
GH025
|
|
1. Model: GH025 HORIZON GYRO-ELECTRIC WITH 14V LED LIGHTED
|
|
Function: Indicating attitude (pitching and banking angles) of an aircraft.
|
|
Specifications:
|
|
Operation Voltage: 14±10% V DC
|
|
Ambient Temperature: -40~+50 ℃
|
|
Relative Humidity: It can reach 95% at 20±5 ℃
|
|
Vibration Strength: not more than 1.5g
|
|
Others: There are 4 pcs LED lights inside instrument, it lighted when it has a power
|
|
Performance:
1. Working Range: Banking 360°, Pitching±70°
2. Accuracy: The indicating error is not more than±1°
3. It will work normally when operation voltage is inputted 3min.and rotor stars and works when 80% operating voltage is below 80% of the rated volt.
4. Operating current is not more than 0.8A.
5. Reference mark should be adjusted in the range of not less than ±5°.
6. The Gyro can return to zero point from any point and lock-in.
7. The insulating resistance between the case is not less than 20MΩ.
8. It is in accordance with the standard of TSO-C4c.
|
|
Model: GH025BL HORIZON GYRO-ELECTRIC 28V WITH LED LIGHTED
|
|
Function: Indicating attitude (pitching and banking angles)of an aircraft.
|
|
Specifications:
|
|
Operation Voltage: 28 ± 10% V DC
|
|
Ambient Temperature: -40~+50 ℃
|
|
Relative Humidity: It can reach 95% at 20±5 ℃
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1. Working Range: Banking 360°, Pitching±70°
2. Accuracy: The indicating error is not more than±1°
3. It will work normally when operation voltage is inputted 3min.and rotor stars and works when 80% operating voltage is below 80% of the rated volt.
4. Operating current is not more than 0.8A.
5. Reference mark should be adjusted in the range of not less than ±5°.
6. The Gyro can return to zero point from any point and lock-in.
7. The insulating resistance between the case is not less than 20MΩ.
8. It is in accordance with the standard of TSO-C4c.
|
|
|
12. Vacuum GYRO
GH030
GD031
|
|
Model: GH030 Vacuum Horizon GYRO
|
|
Function: It is used in a small aircraft to work as an indicating instrument of flying attitude angles of an aircraft
|
|
Features: Pitching angle is within the range of ±70; Banking angle is within the range of 360 degree. It is in accordance with the standard of TSO-C4c
|
|
Specifications:
Ambient temperature: -30 to +50 degree centigrade;
Ambient relative humidity: no more than 95%;
Anti-vibration tensity: 1.5g;
Height: 12000m
Driving power: 15 ~18K Pa for vacuum or air pressure.
Pressure for starting: 7KPa
|
|
Accurany: When an aircraft flies normally, the error is 1 degree.
|
|
SPECIFICATIONS
|
|
SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
GH030
|
|
Indicating attitude (pitching and Banking) of an aircraft.
|
|
Model: GD031 Vacuum Directional GYRO
|
|
Function: It is used in a small aircraft to indicate heading angle of an aircraft.
|
|
Features: Pitching and banking angles are within the range of±70; It is in accordance with the standard of TSO-C5c.
|
|
Specifications:
Air Pressure for Operating: 15~18kPa for vacuum or air pressure
Air pressure for Starting: 7kPa
Ambient temperature: -30~+50℃
Relative Humidity: 0~95%
Vibration strength: not more than 1.5g
Height: 40000 feet
Range for operation: indicates direction within the range of 360o
|
|
Accurant: 4o/10 min
|
|
SPECIFICATIONS
|
|
SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
GD031
|
|
Indicating heading angle of an aircraft.
|
|
|
13. Sideslip Indicator CHY- 1
CHY-1
|
|
Model: CHY-1 SIDESLIP INDICATOR
|
|
Application: Display the aircraft's sideslip motion and help the pilot to control the aircraft to make a turn without sides lip
|
|
Specifications: The indication error is not more than 1.5°when the
black ball center is within 5mm from right and 5mm
from left of center line. The indication error is not
more then 2.5°when the black ball center is beyond the
above mentioned range.
|
|
Ambient temperature: -50℃+70℃
|
|
Altitude:10000m
|
|
Weight: 35g~36g
|
|
|
14. Aircraft Accessories
SCREW TOOLS
|
|
SCREW TOOLS
|
|
ZHUNDA NB(NBD) Preset(set) Torque Wrench Series is a new generation high-quality product,for it combines the advanced military technology with that of other products at home and abroad.And it's also the offspring of our technicians'study and development by absorbing the technology of other similar products,so it has reached the international level.
|
|
The main features: to accuracies of ±4% (meets the international standard), stability, long duration, wide range in use, complete specifications, the changable Ratchet Head. Those over 680 N.M, joined separately, are easy to carry. Both the torque wrenches (from 1N.m-3000N.m) and the torque screwdrivers (from 0.1N.m-6N.m) have met all the customers' needs. Owing to its advantages and unique characteristics, they are now widely used in aviation, aerospace, shipbuilding, autombile, motorcycle, fine mechanics, electric industry, engine, inner-engine and the like, which require high precision in thread components connection.
|
|
ZHUNDA torque wrench is designed and manufactured according to Torque Wrench-General Requirements of GB/T15729 of the national standard of P.R.C and the international standard ISO6789-92.
|
|
|
|
15. Tachometer Series
TACHOMETER
|
|
Model: TACHOMETER SERIES
|
|
SPECIFICATIONS
|
|
SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
L9119
|
0-8,000 PRM
|
2'' SINGLE IG.
|
|
2
|
L9118
|
0-8,000 PRM
|
2'' DUAL IG.
|
|
3
|
L9119A
|
0-8,000 PRM
|
2" BOTH SYSTEM
|
|
4
|
L9121
|
0-8,000 PRM
|
2 1/4 ''SINGLE IG.
|
|
5
|
L9122
|
0-8,000 PRM
|
2 1/4 ''DUAL IG.
|
|
6
|
L9121A
|
0-8,000 PRM
|
2 1/4''BOTH SYSTEM
|
|
7
|
L916
|
0-8,000 PRM
|
3 1/8'' SINGLE IG.
|
|
8
|
L9135
|
0-8,000 PRM
|
3 1/8'' DUAL IG.
|
|
9
|
L916A
|
0-8,000 PRM
|
3 1/8'' BOTHSYSTEM
|
|
|
16. Combined Gauge Series
EGT/TACHO
|
|
SERIAL NO.
|
MODEL NO.
|
MEASURING RANGE
|
DESCRIPTION
|
|
1
|
L203A
|
0-8000RPM/600-1700°F
|
TACHO/EGT 2" SINGLE IG/F.
|
|
2
|
L203B
|
0-8000RPM/600-1700°F
|
TACHO/EGT 2 1/4" SINGLE IG/F.
|
|
3
|
L203C
|
0-8000RPM/600-1700°F
|
TACHO/EGT 3 1/8" SINGLE IG/F.
|
|
4
|
L204A
|
0-8000RPM/600-1700°F
|
TACHO/CHT 2" SINGLE IG/F.
|
|
5
|
L204B
|
0-8000RPM/600-1700°F
|
TACHO/EGT 2 1/4" SINGLE IG/F.
|
|
6
|
L204C
|
0-8000RPM/0-700°F
|
TACHO/CHT 3 1/8" SINGLE IG/F.
|
|
7
|
L9129
|
600-1700°F/0-700°F
|
EGT/CHT 2" FAHR.
|
|
8
|
L9211
|
100-1000°C/0-350°C
|
EGT/CHT 2" CEL.
|
|
9
|
L9116
|
600-1700°F/0-700°F
|
EGT/CHT 2 1/4" FAHR.
|
|
10
|
L9210
|
100-1000°C/0-350°C
|
EGT/CHT 2 1/4" CEL.
|
|
11
|
L209C
|
600-1700°F/0-700°F
|
EGT/CHT 3 1/8" FAHR.
|
|
|
17. Air Data Testing Equipment
ZHY-10
ADT101B
ADTS203D
|
|
Model: ZHY-10 AIR DATA TEST SET
|
|
ZHY-10 air data test set is an intelligent instrument taking vibrating cylinder pressure sensor as its base and high performance single chip microprocessor as its kernel. It working as the reference instrument in the testing and checking of aircraft air pressure instruments including altimeter, combination airspeed indicator, M number indicator, cabin pressure difference indicator, vertical speed indicator, etc.
|
|
Function and Features: · Providing pressure standard
· Self-detection
· Serial communication
· Online correcting
· Metric/English switch
|
|
Specifications:· Pres4sure range:
· total pressure: 10 ～ 2666hPa
· static pressure: 10 ～ 1066hPa
· working temperature: 0 ～ 40 ℃
· Working humidity: relative humidity<90%
· Display mode: VFD fluorescent lattice
· Weight: ≤ 6Kg
|
|
SPECIFICATIONS
|
|
SERIAL NO.
|
PARAMETER
|
MEASURING RANGE
|
ERROR
|
|
1
|
Static pressure (Ps1)
|
8 ～ 800mmHg
|
±0.3mmHg
|
|
2
|
Static pressure (Ps2)
|
10 ～ 1066hPa
|
±0.4hPa
|
|
3
|
Total pressure (Pt1)
|
8 ～ 2000mmHg
|
± 0.4mmHg (8 ～ 800mmHg)
± 0.8mmHg (800 ～ 1800mmHg)
±1.2mmHg (1800 ～ 2000mmHg)
|
|
4
|
Total pressure (Pt2)
|
10 ～ 2666hPa
|
± 0.5hPa (10 ～ 1066hPa)
± 1.1hPa (1066 ～ 2400hPa)
±1.6hPa (2400 ～ 2666hPa)
|
|
5
|
Dynamic pressure (Qc1)
|
0 ～ 1990mmHg
|
± 0.5mmHg (0 ～ 800mmHg)
± 0.9mmHg (800 ～ 1800mmHg)
±1.3mmHg (1800 ～ 1990mmHg)
|
|
6
|
(Qc2)
|
0 ～ 2.7kg. f/cm 2
|
|
|
7
|
(Qc3)
|
0 ～ 27055mmH 2 O
|
|
|
8
|
Height (H)
|
-430 ～ 30000m
|
±5m (0m)
± 16m (9000 ～ 12000m)
±40m (15000m)
±57m (20000m)
|
|
9
|
Indicated airspeed Vi
|
0 ～ 1500km/h
|
±3km/h (350km/h)
±8km/h (1500km/h)
|
|
10
|
True airspeed Vt
|
125 ～ 3000km/h
|
± 10km/h (300 ～ 800km/h)
±20km/h (2000km/h)
±40km/h (2500km/h)
|
|
11
|
Mach number M
|
0 ～3
|
± 0.007 (0.1 ～ 1.5)
± 0.01 (1.5 ～ 3)
|
|
12
|
Indicated M number Mi
|
0 ～ 1.27
|
±0.007
|
|
13
|
Vertical speed H
|
0 ～ 300m/s
|
±0.25m/s (0m/s)
±1m/s (30m/s)
±3m/s (100m/s)
±6m/s (200m/s)
|
|
Model: ADT101B
|
|
Application:· Calibrate ANY Pitot Static Pressure System from helicopters’ to supersonic fighters’.· Test and Verify the accuracy of all kinds of aircraft Pitot Static Instrumentation / Air Data Computers automatically or manually.· Suitable for using with fixed wing and / or rotary aircrafts.· Check aircraft pitot static pressure system for any leakage either at the shop or on the flight line. · Check Flight Instrument: altimeter, ASI, VSI, Mach Meter and air data computer accuracy on the flight line.· Portable, super lightweight, and easy to carry to the shop or the flight line.· Water-proof, moisture-proof, crash-proof and quake-proof case.· Built-in oil-free pressure vacuum pump.· All in one, no additional equipment needed
|
|
Displays: Large screen 151.2 x 34.2mm VFD (vacuum fluorescent display) with dimmer control.
Capability: Altitude - feet, meters.
Airspeed - knots, km/hr Rate of Climb - ft/min, m/s, m/min.
Other Units - mbar, inHg, inH2O, mmHg, kPa, hPa, psi.
Response: 3 readings per second display value updates.
3 readings per second interface and control system updates.
Interface: RS232, RS485 or RS422
Weight: 12 kg / 25 lbs
Dimension: 18.1 ×15 × 7.5in (460 x 380 x 190mm)
Power: AC: 100V~220V at 50~60Hz.
DC: 24V
Operating Temperature: -20 ℃ to + 55℃
|
SPECIFICATIONS
|
|
PARAMETER
|
OPERATING RANGE
|
DISPLAY DIGITS
|
ACCURACY
|
|
Static Sensor
|
10 TO 1310 mbar
(1to38inHg)
|
0.01 mbar
(0.0001 inHg)
|
0.2%full scale
|
|
Pitot Sensor
|
10 to 3500 mbar
(1 to 103 inHg)
|
0.01 mbar
(0.0001 inHg)
|
0.02%full scale
|
|
Altitude
|
-3280ft to +101700ft
|
0.1ft
|
± 2ft at sea level
±7ft at 30,000 ft
±13ft at 60,000ft
|
|
Airspeed
|
11 to 970 knots
|
0 .05 knots
|
± 0.8kts at 50kts
± 0.2kts at 800kts
|
|
Pressure Differential (Dynamic Pressure)
|
0 to 1800 mbar
(0 to 53 in Hg)
Differential
|
0.01 mbar
(0.0001 in Hg)
|
±0.04% full scale
|
|
Rate of Climb
|
0 to 39000 ft/min
|
1 ft/min
|
±1%
|
|
Mach
|
0.1 to 3
|
0.001
|
±0.001
|
|
|
Model: ADTS203D
|
|
Application:
· Calibrate ANY Pitot Static Pressure System from helicopters’ to supersonic fighters’.
· Test and Verify the accuracy of all kinds of aircraft Pitot Static Instrumentation / Air Data Computers automatically or manually.
· Suitable for using with fixed wing and / or rotary aircrafts.
· Check aircraft pitot static pressure system for any leakage either at the shop or on the flight line.
· Check Flight Instrument: altimeter, ASI, VSI, Mach Meter and air data computer accuracy on the flight line
· Portable and easy to carry to the shop or the flight line.
· Water-proof, moisture-proof, crash-proof and quake-proof case.
· Built-in oil-free pressure vacuum pump.
· All in one, no additional equipment needed.
|
|
Displays: Large screen 132 x99mm (5.19” x3.89”) TFT LCD display, super wide
viewable angle. Plus an optional hand held terminal with 72 x54 mm (2.83” x
2.13”) display.
Capability:Altitude - feet, meters
Airspeed - knots, km/hr
Rate of Climb - ft/min, m/s, m/min
Other Units - mbar, inHg, inH2O, mmHg, kPa, hPa, psi.
Response: 3 readings per second display value updates.
3 readings per second interface and control system updates.
Interface: RS232, RS485 or RS422
Weight: 32 kg / 65 lbs
Dimension: 24.6in×19.3in×11.9in (624 mm x 490 mm x 302 mm)
Power: AC: 85V~220V at 43~67Hz
DC: 22V~32V
Operating Temperature: -10 ℃ to + 55℃
|
SPECIFICATIONS
|
|
PARAMETER
|
OPERATING RANGE
|
DISPLAY DIGITS
|
ACCURACY
|
|
Static Sensor
|
10 TO 1310 mbar
(1to38inHg)
|
0.01 mbar
(0.0001 inHg)
|
0.03 mbar
(0.0009 inHg)
|
|
Pitot Sensor
|
10 to 3500 mbar
(1 to 103 inHg)
|
0.01 mbar
(0.0001 inHg)
|
0.03 mbar
(0.0009 inHg)
|
|
Altitude
|
-3280ft to +98000 ft
|
0.1ft
|
± 2ft at sea level
±7ft at 30,000 ft
±13ft at 60,000ft
|
|
Airspeed
|
11 to 970 knots
|
0 .05 knots
|
± 0.8kts at 50kts
± 0.2kts at 800kts
|
|
Pressure Differential (Dynamic Pressure)
|
0 to 1800 mbar
(0 to 53 in Hg)
Differential
|
0.01 mbar
(0.0001 in Hg)
|
±0.04% full scale
|
|
Rate of Climb
|
0 to 39000 ft/min
|
1 ft/min
|
±1%
|
|
Mach
|
0.1 to 3
|
0.001
|
±0.001
|
|
|
+86-0512-62881069
+86-0512-62881069 