- 10 -22.5 +10 - 3.5 +30 15.6
9 -21.6 11 - 2.5 31 16.5
8 -20.6 12 - 1.6 32 17.5
7 -19.7 13 - 0.6 33 18.4
6 -18.7 14 -0.3 34 19.4
5 -17.8 15 1.3 35 20.3
4 -16.8 16 2.2 36 21.3
3 -15.9 17 3.2 37 22.2
2 -14.9 18 4.1 38 23.2
1 -14.0 19 5.1 39 24.1
+ 0 -13.0 20+ 6.0 +40 25.1
1 -12.1 21 7.0
2 -11.1 22 7.9
3 -10.2 23 8.9
4 - 9.2 24 9.9
5 - 8.2 25 10.8
6 - 7.3 26 11.8
7 - 6.3 27 12.7
8 - 5.4 28 13.7
9 - 4.4 29 14.6
CADC P/N HG480C1
Static Air Temperature (`C)
Figure 504
EFFECTIVITY ALL
703 Page 512
34-12-00
Apr 25/87
Test Baro Scale Setting__________________ Altitude Readings_________________
Point_____ (In. Hg)________ (Millibars) (Feet)
(approx)___________
Min___ Max___
1 28.10 952 -1752 -1702
2 28.50 965 -1365 -1315
3 29.00 982 - 888 - 838
4 29.50 999 - 417 - 367
5 29.92 1013 - 25 + 25
6 30.50 1033 + 506 + 556
7 30.90 1046 + 868 + 918
8 31.00 1050 + 958 +1008
Barometric Pressure Setting Error
Figure 505
EFFECTIVITY
799 Page 513
ALL
34-12-00
Aug 25/82
16856
... ............XA
MAX OPER A/S ALTITUDE INDICATED A/S (Knots) STATIC DIFF PITOT (Feet)
(Knots)
(+0/-7) TEST PRESS.PRESS. PRESS.
NORM RES FUEL
POINT(In. Hg)________ (In. Hg)(In. Hg)MODEMODE
0 29.921 0.482 30.403 0 |20 100 |2 377 310
1 29.921 0.949 30.870 0 |20 140 |2 377 310
2 29.921 3.100 33.021 0 |20 250 |3 377 310
3 24.896 8.385 33.281 5000 |35 400 |4 380 310
4 20.577 5.545 26.122 10,000 |50 330 |4 383 310 5 13.7508.385 22.135 20,000 |75 400 |5 394 310 6 8.8856.286 15.17130,000 |100 350 |4 347 310
7 5.538 3.100 8.638 40,000 |125 250 |3 277 277
0 29.921 0.482 30.403 0 |20 100 |2 378 310
1 29.921 0.949 30.870 0 |20 140 |2 378 310
2 29.921 3.100 33.021 0 |20 250 |3 378 310
3 24.896 8.385 33.281 5,000 |35 400 |4 381 310
4 20.577 5.545 26.122 10,000 |50330 |4 384 310 5 13.7508.385 22.135 20,000 |75 400 |5 393 310 6 8.8856.286 15.171 30,000 |100 350 |4345 310
7 5.538 3.100 8.638 40,000 |125 250 |3 276 276
Difference in reading between captain's and first officer's indicators shall not exceed 1-1/2 times the tolerance for the required reading listed for each test. If indicator does not have mode switch, use NORM mode for maximum operating airspeed. (+0/-8) for Vmo limit in AUX FUEL MODE is 342 knots on AF 181-182,197-199 after incorp of SB 28-2119; and LH 014-050 and IB 406-499 after incorp of SB 34-2186 XA ALL EXCEPT LH ALL; AZ 222-229; IB 410-499; plus apls incorp SB 34-2148
Altitude and Airspeed Indicators
Figure 506
EFFECTIVITY ALL
799 Page 514
34-12-00
Aug 25/89
Standard Altitude Static Pressure Altitude Tolerance Test Point (Feet) (In. Hg.) (Feet)
1 25,000 11.104 |75 2 20,000 13.759 |75 3 0 29.921 |30
Hysteresis
Figure 507
Command Reference Test Airspeed Marker Point (Knots) (Knots)
1 110 |1 2 130 |1 3 150 |1 4 180 |1 5 210 |1 6 250 |1 7 260 N/A
Command Airspeed Setting Error
Figure 508
EFFECTIVITYALL
757 Page 515
34-12-00
Aug 25/82
51927
(12)
Measure the resistance of the temperature sensor elements between pins 3 and 4, and 2 and 5.
(13)
Make sure the measured resistance at a given ambient temperature match with the values on the temperature resistance graph (see Figure 511).
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本文鏈接地址：747飛機(jī)維護(hù)手冊AMM CHAPTER 34 - NAVIGATION 第34章導(dǎo)航1(69)
