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DV 20 E AMM
Page 204
15 Mar 2022
34-10-00
Doc # 4.02.25
Rev. 2
C. Low Range Static Leak Test
Detail Steps/Work Items
Key Items/References
(1)
Obey the precautions at the beginning of this
subject.
(2)
Connect the pitot-static leak-tester to the pitot-
static probe.
(3)
Apply a partial vacuum to the static port until
you get a pressure altitude of 1000 ft above the
ambient pressure altitude.
Note the altitude.
(4)
Let the pressure stabilize.
(5)
Monitor the system pressure.
The pressure loss must not be more
than 100 ft/min.
(6)
Compare the test-equipment altimeter and the
airplane altimeter.
Table 1: Altimeter Indication Error
Altitude
Permissible Error
Sea level.
±20 ft.
4,000 ft.
±35 ft.
8,000 ft.
±60 ft.
12,000 ft.
±90 ft.
16,000 ft.
±110 ft.
20,000 ft.
±130 ft.
Summary of Contents for DV 20 E 2022
Page 50: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 4 15 Mar 2022 04 00 00 Doc 4 02 25 Rev 2...
Page 405: ...AIRCRAFT DV 20 E AMM Fuel Doc 4 02 25 Rev 2 28 TITLE Page 1 15 Mar 2022 CHAPTER 28 FUEL...
Page 561: ...AIRCRAFT DV 20 E AMM Lights Doc 4 02 25 Rev 2 33 TITLE Page 1 15 Mar 2022 CHAPTER 33 LIGHTS...
Page 679: ...AIRCRAFT DV 20 E AMM Doors Doc 4 02 25 Rev 2 52 TITLE Page 1 15 Mar 2022 CHAPTER 52 DOORS...
Page 686: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Figure 1 Canopy...
Page 741: ...AIRCRAFT DV 20 E AMM Windows Doc 4 02 25 Rev 2 56 TITLE Page 1 15 Mar 2022 CHAPTER 56 WINDOWS...
Page 757: ...AIRCRAFT DV 20 E AMM Wings Doc 4 02 25 Rev 2 57 TITLE Page 1 15 Mar 2022 CHAPTER 57 WINGS...
Page 857: ...AIRCRAFT DV 20 E AMM Exhaust Doc 4 02 25 Rev 2 78 TITLE Page 1 15 Mar 2022 CHAPTER 78 EXHAUST...
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