You should also add the template to the talk page.A model attribution edit summary is Content in this edit is translated from the existing Russian Wikipedia article at ] see its history for attribution. You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation.If possible, verify the text with references provided in the foreign-language article. Do not translate text that appears unreliable or low-quality.Consider adding a topic to this template: there are already 2,536 articles in the main category, and specifying |topic= will aid in categorization.Machine translation like DeepL or Google Translate is a useful starting point for translations, but translators must revise errors as necessary and confirm that the translation is accurate, rather than simply copy-pasting machine-translated text into the English Wikipedia.The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. ![]() ![]() The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. ![]() The test point shall then be approached at a rate of approximately 3,000 feet per minute. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i) and while the altimeter is at this pressure, the hysteresis test shall commence. Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections Recording of Major Repairs and Major Alterations Major Alterations, Major Repairs, and Preventive Maintenance aeronautical products by certain Canadian persons. Maintenance, preventive maintenance, and alterations performed on U.S. Maintenance records: Falsification, reproduction, or alteration.Īdditional performance rules for inspections. ![]() Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration.Ĭontent, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, § 135.411(a)(1), and § 135.419 of this chapter).ĭisposition of life-limited aircraft parts.Ĭontent, form, and disposition of records for inspections conducted under parts 91 and 125 and §§ 135.411(a)(1) and 135.419 of this chapter. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations.Īpproval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Maintenance, Preventive Maintenance, Rebuilding, and Alteration
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