V46 航空器試驗(yàn)設(shè)備 標(biāo)準(zhǔn)查詢與下載
共找到 35 條與 航空器試驗(yàn)設(shè)備 相關(guān)的標(biāo)準(zhǔn)，共 3 頁
本文件規(guī)定了無人機(jī)綜合驗(yàn)證場(chǎng)的等級(jí)劃分,以及各等級(jí)驗(yàn)證場(chǎng)的場(chǎng)地條件、系統(tǒng)設(shè)備、 實(shí)驗(yàn)檢校配置、專業(yè)人員配置等要求。 本文件適用于遙感與測(cè)繪無人機(jī)綜合驗(yàn)證場(chǎng)的設(shè)計(jì)、建設(shè)和評(píng)估。其他應(yīng)用領(lǐng)域的無人 機(jī)驗(yàn)證場(chǎng)可參考使用。
General requirements for UAV comprehensive verification field
- ICS
- 49.100
- CCS
- V46
- 發(fā)布
- 2021-03-22
- 實(shí)施
- 2021-03-22
(a) Except as provided in this paragraph, each person on board an aircraftoperated under this part shall occupyan approved seat or berth with a separate safety belt properly secured abouthim or her during movement on thesurface, takeoff, and landing. For seaplane and float equipped rotorcraft operations during movement on the surface, the person pushing off the seaplane or rotorcraft from the dock andthe person mooring the seaplane orrotorcraft at the dock are exceptedfrom the preceding seating and safetybelt requirements. A safety belt provided for the occupant of a seat maynot be used by more than one personwho has reached his or her secondbirthday. Notwithstanding the preceding requirements, a child may
Aeronautics and Space. Part135:Operating requirements: Commuter and on demand operations and rules governing persons on board such aircraft. Section135.128:Use of safety belts and child restraint systems.
- ICS
- CCS
- V46
- 發(fā)布
- 2014-05-20
- 實(shí)施
- 2014-05-20
(a) After April 24, 2017, no person mayoperate a rotorcraft unless that rotorcraft is equipped with an operableFAA-approved radio altimeter, or anFAA-approved device that incorporatesa radio altimeter, unless otherwise authorized in the certificate holder’s approved minimum equipment list.
Aeronautics and Space. Part135:Operating requirements: Commuter and on demand operations and rules governing persons on board such aircraft. Section135.160:Radio altimeters for rotorcraft operations.
- ICS
- CCS
- V46
- 發(fā)布
- 2014-02-21
- 實(shí)施
- 2015-04-22
本規(guī)范規(guī)定了靜壓液浮陀螺平臺(tái)系統(tǒng)（以下簡(jiǎn)稱平臺(tái)系統(tǒng))要求、質(zhì)量保證規(guī)定和交貨準(zhǔn)備。 本規(guī)范適用于平臺(tái)系統(tǒng)的設(shè)計(jì)、生產(chǎn)、試驗(yàn)與檢驗(yàn)。
General specification for hydrostatic liquid-bearing gyro platform system
- ICS
- CCS
- V46
- 發(fā)布
- 2011-07-19
- 實(shí)施
- 2011-10-01
本標(biāo)準(zhǔn)規(guī)定了靜壓液浮陀螺平臺(tái)系統(tǒng)測(cè)試的-般要求、測(cè)試項(xiàng)目、測(cè)試及檢查方法。 本標(biāo)準(zhǔn)適用于靜壓液浮陀螺平臺(tái)系統(tǒng)（以下簡(jiǎn)稱平臺(tái)系統(tǒng)）的測(cè)試。其它慣性儀表及平臺(tái)系統(tǒng)的測(cè)試可參照使用。
Test method for hydrostatic liquid-bearing gyro platform system
- ICS
- CCS
- V46
- 發(fā)布
- 2011-07-19
- 實(shí)施
- 2011-10-01
This SAE Aerospace Recommended Practice (ARP) specifies a series of balancing machine provingrotors and related test weights as directly required for the evaluation of gas turbine rotor balancingmachines.1.1 Purpose:Provides the recommended design for the construction of balancing machine proving rotors.
Balancing Machine Proving Rotors
- ICS
- CCS
- V46
- 發(fā)布
- 2011-07-01
- 實(shí)施
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的RD-AX8340型航椅測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of Model RD-AX8340 Seat Tester
- ICS
- CCS
- V46
- 發(fā)布
- 2006-08-28
- 實(shí)施
- 2006-12-01
本規(guī)范適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的件號(hào)為J32001的剎車踏板測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的校準(zhǔn)。
Calibration Specification of Brake Pedal Measuring Equipment
- ICS
- CCS
- V46
- 發(fā)布
- 2006-08-17
- 實(shí)施
- 2006-12-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的682003006型、682003007型和682003008型沖壓渦輪測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of Model 682003006/7/8 Ground Check Electrical Unit
- ICS
- CCS
- V46
- 發(fā)布
- 2006-08-17
- 實(shí)施
- 2006-12-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的HCS9000B/HCS9200B型復(fù)合材料熱補(bǔ)儀（以下簡(jiǎn)稱熱補(bǔ)儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of Model HCS9000B/HCS9200B Composite Repair Controller/Hot Bonder
- ICS
- CCS
- V46
- 發(fā)布
- 2006-08-17
- 實(shí)施
- 2006-12-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的ADTS405/405F型大氣數(shù)據(jù)測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of Model ADTS405/405F Air Data Test Systems
- ICS
- CCS
- V46
- 發(fā)布
- 2006-08-17
- 實(shí)施
- 2006-12-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的906-10247-2型環(huán)路電阻測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of 906-10247-2 Loop Resistance Tester
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-23
- 實(shí)施
- 2006-09-01
本規(guī)程適用于民用航空飛機(jī)維修中應(yīng)用的101-5HJ點(diǎn)火電路測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。同系列測(cè)試儀可參考本規(guī)程。
Verification Regulation of 101-5HJ Igniter Circuit Tester
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-23
- 實(shí)施
- 2006-09-01
本規(guī)程適用于民用航空飛機(jī)維修中應(yīng)用的V2500引氣活門測(cè)試儀（以下簡(jiǎn)稱測(cè)試儀）的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of V2500 Bleed Valve Test Set
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-23
- 實(shí)施
- 2006-09-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的AC30-60型飛機(jī)稱重平臺(tái)的首次檢定、后續(xù)檢定和使用中的檢驗(yàn)。
Verification Regulation of AC30-60 Aircraft Weighing Platform
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-23
- 實(shí)施
- 2006-09-01
本規(guī)程適用于民用航空系統(tǒng)飛機(jī)維修中應(yīng)用的直讀式渦流電導(dǎo)率測(cè)試儀的首次檢定、后續(xù)檢定和使用中檢驗(yàn)。
Verification Regulation of Eddy Current Conductivity Meter
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-23
- 實(shí)施
- 2006-09-01
本標(biāo)準(zhǔn)規(guī)定了航空渦噴渦扇發(fā)動(dòng)機(jī)地面試車臺(tái)和航空渦槳渦軸發(fā)動(dòng)機(jī)地面試車臺(tái)（以下簡(jiǎn)稱為試車臺(tái)）的設(shè)計(jì)、驗(yàn)收、校準(zhǔn)和使用維護(hù)要求。 本標(biāo)準(zhǔn)適用于新建、改建和對(duì)發(fā)動(dòng)機(jī)性能測(cè)試有影響的修理的室內(nèi)、露天以及進(jìn)行可變分力試驗(yàn)的試車臺(tái)。
General requirement for aero-turbo engine ground test bed
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-17
- 實(shí)施
- 2006-10-01
本標(biāo)準(zhǔn)規(guī)定了軍用直升機(jī)地面聯(lián)合試車臺(tái)試驗(yàn)要求。 本標(biāo)準(zhǔn)適用于各類軍用直升機(jī)的地面聯(lián)合試車臺(tái)試驗(yàn)，可作為其設(shè)計(jì)符合性驗(yàn)證、首飛及試驗(yàn)相關(guān)系統(tǒng)的依據(jù)。
General requirements for military helicopter joint bench test
- ICS
- CCS
- V46
- 發(fā)布
- 2006-05-17
- 實(shí)施
- 2006-10-01
This SAE Aerospace Recommended Practice (ARP) document provides recommended practices for the calibration and acceptance of icing wind tunnels to be used in testing ofaircraft components and systems and for the development of simulated ice shapes. Thisdocument is not applicable to air-breathing propulsion test facilities configured for thepurposes of engine icing tests. Use of facilities as part of an aircraft?s ice protectionCertification Plan should be reviewed and accepted by the applicable regulatory agencyprior to testing. Following acceptance of a test plan, data generated in these facilities maybe submitted to regulatory agencies for use in the certification of aircraft ice protectionsystems and components. Certain types of tests may be appropriate in facilities withcapabilities that are not as rigorously characterized as by the practices defined herein, andthe acceptability of these tests should be coordinated with the applicable regulatory agency.
Calibration and Acceptance of Icing Wind Tunnels
- ICS
- 49.045
- CCS
- V46
- 發(fā)布
- 2003-09-01
- 實(shí)施
The purpose of this recommended practice document is to provide the reader with increased knowledge about planning and executing highly successful wind tunnel tests. First, an overview of the test process is provided, giving a general picture of the origin, purpose, and high-level breakdown of activities that are a part of wind tunnel test development and execution. Secondly, detail is added to the overview to define the full scope of the activities and key considerations. Finally, recommended practices and lessons learned are described.
Wind Tunnel Testing Part 2: Practitioners Volume
- ICS
- CCS
- V46
- 發(fā)布
- 2003-01-01
- 實(shí)施
