|
|
1. Barometric
Altimeter
BG-3E

BG-3H

BG10-2

BG3
|
|
|
|
Model: BG-3 SERIES
|
|
Application: It is used to measure the relative altitude of an
aircraft in flight.
|
|
Measuring Range: -1000~20,000ft
|
|
Operation Temperature: -30~+50¡æ
|
|
Indication accuracy: conforms to As 392c
|
|
Dimension: 82.5 x 105
|
|
Weight: <700g
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BG-3
|
28.1~31.0 inHg, -1000~20,000ft
|
3-pointer, ten thousand pointer in plate
form 3 1/8"
|
|
2
|
BG-3A
|
950~1,050Mbar,
-1000~20,000ft
|
3-pointer, ten thousand pointer in plate
form 3 1/8"
|
|
3
|
BG-3B
|
28.1~31.0 inHg, -1000~20,000ft
|
3-pointer, 3 1/8"
|
|
4
|
BG-3E
|
950~1,050Mbar,
-1000~20,000ft
|
3-pointer, 3 1/8"
|
|
5
|
BG-3H
|
-1000~20,000ft,
950~1,050Mbar, 28.1~31.0 inHg
|
Two baro-windows,
3-pointer, 3 1/8"
|
|
Model: BG-7 SERIES
|
|
Application: It is used to indicate the relative altitude of an
aircraft, fitting for sports
gliders.
|
|
Measuring Range: 0~5,500ft
|
|
Max Measurement: 12,000ft
|
|
Barometric Scale Range: 28~31
inHg
|
|
Operation Temperature: -20~+50¡æ
|
|
Dimension: 82.5 x 82.5 x 73
|
|
Weight: <350g
|
|
Specifications: single pointer
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BG-7
|
0~5,500ft, 28~31 inHg
|
3 1/8"
|
|
2
|
BG-12A
|
0~5,500ft,
50~1,050Mbar
|
3 1/8"
|
|
Model: BG-11 SERIES
|
|
Application: It is used to indicate the relative altitude of an
aircraft, fitting for sports
gliders.
|
|
Measuring Range: 0~10,000ft
|
|
Barometric Scale Range: 28~31
inHg
|
|
Operation Temperature: -20~+50¡æ
|
|
Dimension: 82.5 x 82.5 x 73
|
|
Weight: <350g
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BG-11
|
0~10,000ft, 28~31
inHg
|
3 1/8"
|
|
2
|
BG-11A
|
0~10,000ft,
950~1,050Mbar
|
3 1/8"
|
|
3
|
BG-11B
|
0~300m,
950~1,050Mbar
|
3 1/8"
|
|
Model: Single-Pointer Altimeter
|
|
Application: It is used to indicate the relative altitude of an
aircraft in the flight.
|
|
Operation Temperature: -30~+50¡æ
|
|
Dimension: 60 x 60 x 109
|
|
Weight: <120g
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BG-9
|
0~5,000ft, 27~31 inHg
|
2 1/4"cut
out (¦µ57x78.5)
|
|
2
|
BG-10
|
0~10,000ft, 27~31
inHg
|
2 1/4"cut
out (¦µ57x78.5)
|
|
3
|
BG-15
|
0~10,000ft, 27~31
inHg
|
2 1/4"cut
out (¦µ57x78.5)
|
|
4
|
BG3
|
0~3,000m,
910~1,050Mbar
|
2 1/4"cut
out (¦µ57x78.5)
|
|
5
|
BG6-1A
|
0~6,000m,
900~1,050Mbar
|
2 1/4"cut
out (¦µ57x78.5)
|
|
6
|
BG6-2
|
0~6,000m,
700~1,040Mbar
|
3 1/8"cut
out (¦µ80x52.6)
|
|
7
|
BG-14
|
0~6,000m,
900~1,050Mbar
|
2 1/4"cut
out
|
|
8
|
BG10-2
|
0~10,000m,
600~1,040Mba
|
3 1/8"cut
out (¦µ80x52.5)
|
|
|
2. Accelerometer
("G" Meter)

BJ10-2F
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BJ10-2F
|
-5~+10g
|
2 1/4"cut
out
|
|
|
3. Manifold Pressure
Indicator

BYJ-3
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BYJ-3
|
10~50 inHg
|
3 1/8"cut
out
|
|
|
4. Oil Temperature
and Pressure Indicator
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BWY-8
|
0~100Ib/in, 40~28¨H, 4.4~137.88¡æ
|
3 1/8"cut
out
|
|
|
5. Airspeed indicator

BK150-1A

BK-240

BK-7B

BK300
|
|
Application: It is used to measure the indicated airspeed of an
aircraft.
|
|
Operation Temperature: -20~+50¡æ
|
|
Indicating Accurace: conforming
to AS8019
|
|
Weight: <350g
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BK-3
|
20-160mph, 20-140
knots
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
2
|
BK-3A
|
20-140 knots
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
3
|
BK-4
|
30-180mph,
30-160 knots
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
4
|
BK-5
|
30-250mph,30-220
knots
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
5
|
BK-5A
|
30-220knot
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
6
|
BK-10
|
30-200mph,
30-180knots
|
3 1/8''Cut out (¦µ79.4 x 97.3)
|
|
7
|
BK-11
|
30-200mph,
30-170knots
|
3
1/8" (¦µ80 x 58) out.:mph, inside.:knots
|
|
8
|
BK-11A
|
30-200mph,
30-170knots
|
3
1/8" (¦µ80 x 58) out.:knots, inside.:mph
|
|
9
|
BK-9C
|
20-8
mph
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
10
|
BK-8D
|
20-100mph
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
11
|
BK-7B
|
20-120mph
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
12
|
BK-6C
|
20-150mph
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
13
|
BK-12
|
20-80knots
|
3
1/8" (¦µ80 x 58)
|
|
14
|
BK-13A
|
20-100knots
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
15
|
BK-14A
|
20-120knots
|
3
1/8" (¦µ80 x 58) Dense
scale
|
|
16
|
BK-40
|
20-250knots
|
3
1/8" (¦µ80 x 58)
|
|
17
|
BK-15
|
20-160knots
|
3
1/8" (¦µ79.4 x 97.3)
|
|
18
|
BK-25
|
40-260knots
|
3
1/8" (¦µ79.4 x 97.3)
|
|
19
|
BK120-1B
|
30-120kph
|
3
1/8" (¦µ80 x 58)
|
|
20
|
BK150-1A
|
30-150kph
|
3
1/8" (¦µ80 x 58)
|
|
21
|
BK200-1A
|
30-200kph
|
3
1/8" (¦µ80 x 58)
|
|
22
|
BK240
|
30-240kph
|
3
1/8" (¦µ80 x 58)
|
|
23
|
BK300
|
30-300kph
|
3
1/8" (¦µ80 x 58)
|
|
24
|
BK-31
|
20-140mph
|
3
1/8" (¦µ80 x 97)
|
|
25
|
BK-32
|
20-160mph
|
3
1/8" (¦µ80 x 97)
|
|
26
|
BK-33
|
30-180mph
|
3
1/8" (¦µ80 x 97)
|
|
27
|
BK-34
|
30-180mph
|
3
1/8" (¦µ80 x 97)
|
|
28
|
BK-35
|
30-200mph
|
3
1/8" (¦µ80 x 97)
|
|
29
|
BK-36
|
20-80mph
|
2
1/4" cut out (¦µ57 x 60) with 0
scale
|
|
30
|
BK-37
|
20-100mph
|
2
1/4" cut out (¦µ57 x 60) with 0
scale
|
|
31
|
BK-38
|
20-120mph
|
2
1/4" cut out (¦µ57 x 60) with 0
scale
|
|
32
|
BK-20
|
20-80mph
|
2
1/4" cut out (¦µ57 x 60) no 0
scale
|
|
33
|
BK-21
|
20-100mph
|
2
1/4" cut out (¦µ57 x 60) no 0
scale
|
|
34
|
BK-22
|
20-120mph
|
2
1/4" cut out (¦µ57 x 60) no 0
scale
|
|
35
|
BK-23
|
20-140mph
|
2
1/4" cut out (¦µ57 x 60) no 0
scale
|
|
36
|
BK-42
|
20-140mph
|
2
1/4" cut out (¦µ57 x 60) with 0
scale
|
|
|
6. Vertical Speed Indicator

BC-2A

BC10-1B

BC-6A
|
|
Application: It is used to indicate the vertical speed of an
aircraft.
|
|
Operation Temperature: -20~+50¡æ
|
|
Indicating Accurace: conforming
to TSO-C8C (AS8016)
|
|
Weight: <500g
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
BC-3
|
0~+/-3,000
ft/min
|
Figure outside,
scale inside,
3 1/8"cut
out
|
|
2
|
BC-4
|
0~+/-4,000
ft/min
|
Figure outside,
scale inside,
3 1/8"cut
out
|
|
3
|
BC-2A
|
0~+/-2,000
ft/min
|
Figure outside,
scale inside,
3 1/8"
inside, 3 1/8"cut out
|
|
4
|
BC-6
|
0~+/-2,000
ft/min
|
Figure outside,
scale inside,
2 1/4" cut
out outside,
2 1/4"cut
out
|
|
5
|
BC-6A
|
0~+/-10
m/s
|
2 1/4''Cut out
|
|
6
|
BC-10-1B
|
0~+/-10
m/s
|
3 1/8''Cut out
|
|
|
7. Engine
Instruments

EGT/EGT

EGT
PROBES

CHT/CHT2

CHT PROBES

WATER
TEMP. GAUGE

VOLTMETER
|
|
Model: EGT SERIES
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
L9114
|
600-1,700¡ãF/100-1000¡ãC
|
EGT 2"
FAHR./CEL
|
|
2
|
L9218
|
600-1,700¡ãF
|
EGT 2" FAHR.
|
|
3
|
L9219
|
100-1000¡ãC
|
EGT
2'' CEL.
|
|
4
|
L917
|
600-1700¡ãF/100-1000¡ãC
|
EGT
2 1/4'' FAHR./CEL.
|
|
5
|
L928
|
600-1700¡ãF
|
EGT
2 1/4'' FAHR.
|
|
6
|
L929
|
100-1000¡ãC
|
EGT
2 1/4'' CEL
|
|
7
|
L205C
|
600-1700¡ãF
|
EGT
3 1/8'' FAHR.
|
|
8
|
L9126
|
600-1700¡ãF
|
EGT/EGT
2'' FAHR
|
|
9
|
L9214
|
100-1000¡ãC
|
EGT/EGT
2'' CEL.
|
|
10
|
L9127
|
600-1700¡ãF
|
EGT/EGT
2 1/4'' FAHR.
|
|
11
|
L9215
|
100-1000¡ãC
|
EGT/EGT
2 1/4'' CEL.
|
|
12
|
L207C
|
600-1705¡ãF
|
EGT/EGT
3 1/8'' FAHR.
|
|
13
|
L912A
|
M
8X1 SCREW TYPE
|
EGT
PROBES
|
|
14
|
L912B
|
Z
1/8 SCREW TYPE
|
EGT
PROBES
|
|
Model: CHT SERIES
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
L918
|
0-700¡ãF/0-350¡ãC
|
CHT
2'' FAHR./CEL.
|
|
2
|
L926
|
0-700¡ãF
|
CHT
2'' FAHR.
|
|
3
|
L927
|
0-350¡ãC
|
CHT
2'' CEL.
|
|
4
|
L9125
|
0-700¡ãF/0-350¡ãC
|
CHT
2 1/4'' FAHR./CEL.
|
|
5
|
L9216
|
0-700¡ãF
|
CHT
2 1/4'' FAHR.
|
|
6
|
L92177
|
0-350¡ãC
|
CHT
2 1/4'' CEL.
|
|
7
|
L206C
|
0-700¡ãF
|
CHT
3 1/8'' FAHR.
|
|
8
|
L9124
|
0-700¡ãF
|
CHT/CHT
2'' FAHR.
|
|
9
|
L9213
|
0-350¡ãC
|
CHT/CHT
2'' CEL.
|
|
10
|
L9123
|
0-700¡ãF
|
CHT/CHT
2 1/4'' FAHR.
|
|
11
|
L9212
|
0-350¡ãC
|
CHT/CHT
2 1/4'' CEL
|
|
12
|
L208C
|
0-700¡ãF
|
CHT/CHT
3 1/8'' FAHR.
|
|
13
|
L913C
|
14MM
METAL SLEEVE
|
CHT
PROBES
|
|
14
|
L913E
|
10MM
METAL SLEEVE
|
CHT
PROBES
|
|
15
|
L913D
|
12MM
METAL SLEEVE
|
CHT
PROBES
|
|
16
|
L913B
|
18MM
METAL SLEEVE
|
CHT
PROBES
|
|
Model: WATER TEMP. GAUGE SERIES
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
L9128A
|
100-250¡ãF/40-120¡ãC
|
2''
FAHR./CEL.
|
|
2
|
L9128
|
100-250¡ãF/40-120¡ãC
|
2
1/4'' FAHR.
|
|
3
|
L210C
|
100-250¡ãF/40-120¡ãC
|
3
1/8'' CEL.
|
|
Model: VOLTMETER SERIES
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
L211A
|
6-16V
|
2''
|
|
2
|
L211B
|
6-16V
|
2
1/4''
|
|
3
|
L211C
|
6-16V
|
3
1/8''
|
|
|
8. Compass

CM-13

CM-24

MC-022
|
|
Model: CM-13, CM-13L MAGNETIC COMPASS (LIQUID COMPASS)
|
|
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).
|
|
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 ¡æ
5. It is in accordance with the standard of TSO-C7d.
|
|
SPECIFICATIONS
|
|
SERIAL
NO.
|
MODEL
NO.
|
MEASURING
RANGE
|
DESCRIPTION
|
|
1
|
CM-13
|
|
|
|
Model: CM-24
|
|
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)
|
|
Specifications: When the compass
compensation is adjusted to neutral position, the error of the compass is ¡À2.5 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.
|
|
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.
|
|
SPECIFICATIONS
|
|
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.
|
|
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¡À1% V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20¡À5 ¡æ
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1.
Working Range: Indicating heading angle within the range of 360¡ã
2.
Accuracy: The drift error is not more than 4¡ã/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 M¦¸.
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¡À1% V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20¡À5 ¡æ
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1.
Working Range: Indicating heading angle within the range of 360¡ã
2.
Accuracy: The drift error is not more than 4¡ã/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 M¦¸.
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 ¡À1%V
|
|
Ambient Temperature: -40~+50
|
|
Relative Humidity: It can reach 95% at 20¡À5 ¡æ
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1.
Working Range: Indicating heading angle within the range of 360¡ã
2.
Accuracy: The drift error is not more than 4¡ã/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 M¦¸.
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¡À10% V DC
|
|
Ambient Temperature: -40~+50 ¡æ
|
|
Relative Humidity: It can reach 95% at 20¡À5 ¡æ
|
|
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¡ã,
Pitching¡À70¡ã
2.
Accuracy: The indicating error is not more than¡À1¡ã
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 ¡À5¡ã.
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 20M¦¸.
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 ¡À 10% V DC
|
|
Ambient Temperature: -40~+50 ¡æ
|
|
Relative Humidity: It can reach 95% at 20¡À5 ¡æ
|
|
Vibration Strength: not more than 1.5g
|
|
Performance:
1.
Working Range: Banking 360¡ã,
Pitching¡À70¡ã
2.
Accuracy: The indicating error is not more than¡À1¡ã
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 ¡À5¡ã.
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 20M¦¸.
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 ¡À70;
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¡À70; 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¡æ
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¡ãwhen 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¡ãwhen the black
ball center is beyond the
above mentioned range.
|
|
Ambient temperature: -50¡æ+70¡æ
|
|
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 ¡À4% (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¡ãF
|
TACHO/EGT 2" SINGLE IG/F.
|
|
2
|
L203B
|
0-8000RPM/600-1700¡ãF
|
TACHO/EGT 2 1/4" SINGLE IG/F.
|
|
3
|
L203C
|
0-8000RPM/600-1700¡ãF
|
TACHO/EGT 3 1/8" SINGLE IG/F.
|
|
4
|
L204A
|
0-8000RPM/600-1700¡ãF
|
TACHO/CHT 2" SINGLE IG/F.
|
|
5
|
L204B
|
0-8000RPM/600-1700¡ãF
|
TACHO/EGT 2 1/4" SINGLE IG/F.
|
|
6
|
L204C
|
0-8000RPM/0-700¡ãF
|
TACHO/CHT 3 1/8" SINGLE IG/F.
|
|
7
|
L9129
|
600-1700¡ãF/0-700¡ãF
|
EGT/CHT 2" FAHR.
|
|
8
|
L9211
|
100-1000¡ãC/0-350¡ãC
|
EGT/CHT 2" CEL.
|
|
9
|
L9116
|
600-1700¡ãF/0-700¡ãF
|
EGT/CHT 2 1/4" FAHR.
|
|
10
|
L9210
|
100-1000¡ãC/0-350¡ãC
|
EGT/CHT 2 1/4" CEL.
|
|
11
|
L209C
|
600-1700¡ãF/0-700¡ãF
|
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 ¡æ
¡¤
Working humidity: relative humidity<90%
¡¤ Display mode: VFD fluorescent lattice
¡¤ Weight: ¡Ü 6Kg
|
|
SPECIFICATIONS
|
|
SERIAL NO.
|
PARAMETER
|
MEASURING RANGE
|
ERROR
|
|
1
|
Static pressure (Ps1)
|
8 ¡« 800mmHg
|
¡À0.3mmHg
|
|
2
|
Static pressure (Ps2)
|
10 ¡« 1066hPa
|
¡À0.4hPa
|
|
3
|
Total pressure (Pt1)
|
8 ¡« 2000mmHg
|
¡À 0.4mmHg (8 ¡«
800mmHg)
¡À 0.8mmHg (800 ¡«
1800mmHg)
¡À1.2mmHg (1800 ¡« 2000mmHg)
|
|
4
|
Total pressure (Pt2)
|
10 ¡« 2666hPa
|
¡À 0.5hPa (10 ¡«
1066hPa)
¡À 1.1hPa (1066 ¡« 2400hPa)
¡À1.6hPa (2400 ¡«
2666hPa)
|
|
5
|
Dynamic pressure (Qc1)
|
0 ¡« 1990mmHg
|
¡À 0.5mmHg (0 ¡«
800mmHg)
¡À 0.9mmHg (800 ¡« 1800mmHg)
¡À1.3mmHg (1800 ¡«
1990mmHg)
|
|
6
|
(Qc2)
|
0 ¡« 2.7kg. f/cm 2
|
|
|
7
|
(Qc3)
|
0 ¡« 27055mmH 2 O
|
|
|
8
|
Height (H)
|
-430 ¡« 30000m
|
¡À5m (0m)
¡À 16m (9000 ¡«
12000m)
¡À40m (15000m)
¡À57m (20000m)
|
|
9
|
Indicated airspeed Vi
|
0 ¡« 1500km/h
|
¡À3km/h (350km/h)
¡À8km/h (1500km/h)
|
|
10
|
True airspeed Vt
|
125 ¡« 3000km/h
|
¡À 10km/h (300 ¡« 800km/h)
¡À20km/h (2000km/h)
¡À40km/h (2500km/h)
|
|
11
|
Mach number M
|
0 ¡«3
|
¡À 0.007 (0.1 ¡«
1.5)
¡À 0.01 (1.5 ¡« 3)
|
|
12
|
Indicated M number Mi
|
0 ¡« 1.27
|
¡À0.007
|
|
13
|
Vertical speed H
|
0 ¡« 300m/s
|
¡À0.25m/s (0m/s)
¡À1m/s (30m/s)
¡À3m/s (100m/s)
¡À6m/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 ¡Á15 ¡Á
7.5in (460 x 380 x 190mm)
Power: AC:
100V~220V at 50~60Hz.
DC:
24V
Operating Temperature: -20
¡æ to + 55¡æ
|
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
|
¡À
2ft at sea level
¡À7ft
at 30,000 ft
¡À13ft
at 60,000ft
|
|
Airspeed
|
11 to 970 knots
|
0
.05 knots
|
¡À
0.8kts at 50kts
¡À 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)
|
¡À0.04%
full scale
|
|
Rate
of Climb
|
0
to 39000 ft/min
|
1 ft/min
|
¡À1%
|
|
Mach
|
0.1
to 3
|
0.001
|
¡À0.001
|
|
|
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¡Á19.3in¡Á11.9in
(624 mm x 490 mm x 302 mm)
Power: AC:
85V~220V at 43~67Hz
DC: 22V~32V
Operating Temperature: -10
¡æ to + 55¡æ
|
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
|
¡À
2ft at sea level
¡À7ft
at 30,000 ft
¡À13ft
at 60,000ft
|
|
Airspeed
|
11 to 970 knots
|
0
.05 knots
|
¡À
0.8kts at 50kts
¡À 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)
|
¡À0.04%
full scale
|
|
Rate
of Climb
|
0
to 39000 ft/min
|
1 ft/min
|
¡À1%
|
|
Mach
|
0.1
to 3
|
0.001
|
¡À0.001
|
|
|