(iii) "After effect"
Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II.
(iv) "Friction."
The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III.
(v) "Case leak."
The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute.
(vi) "Barometric scale error."
At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet.
(6) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator.
III. Integration Test
Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet.
IV. Records:
Comply with the provisions of the fifth Schedule as to content, form, and disposition of the records. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record.
TABLE I TO APPENDIX 1 TO 5.105: ALTITUDE & EQUIVALENT BAROMETRIC PRESSURE
Altitude Equivalent pressure (inches of Mercury) Tolerance ±(feet)
-1,000 31.018 20
0 29.921 20
500 29.385 20
1,000 28.856 20
1,500 28.335 25
2,000 27.821 30
3,000 26.817 30
4,000 25.842 35
6,000 23.978 40
8,000 22.225 60
10,000 20.577 80
12,000 19.029 90
14,000 17.577 100
16,000 16.216 110
18,000 14.942 120
20,000 13.750 130
22,000 12.636 140
25,000 11.104 155
30,000 8.885 180
35,000 7.041 205
40,000 5.538 230
45,000 4.355 255
50,000 3.425 280
TABLE II TO APPENDIX 1 TO 5.105: TEST TOLERANCES
Test Tolerance (feet)
Case Leak Test ±100
Hysteresis Test
- First Test Point (50 percent of maximum altitude) +75
- Second Test Point (40 percent of maximum altitude) +75
After Effect Test +30
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