Procurando um bd 5 aircraft specifications pdf online? FilesLib está aqui para ajudá-lo a economizar o tempo gasto na pesquisa. Os resultados da pesquisa incluem nome do arquivo, descrição, tamanho e número de páginas. Você pode ler bd 5 aircraft specifications pdf online ou faça o download para o seu computador.

1962 - Legendary designer James Bede designs the forerunner to today's Tiger—the BD-1, a two-seater with interchangeable wings and horizontal stabilizer components. 1964 - Bede sells the BD-1 design to American Aviation and stays on as a consultant for the production of the plane. range, high altitude, and high-speed business/corporate aircraft. With a range of 3100 NM at 0.83M and a 45,000 ft maximum operating altitude at initial certification, the aircraft has been designed for mission duration up to 7 hours. Two Honeywell AS907 turbofan engines with reverse thrust capability are rear fuselage mounted on pylons. Part 21. Approval of part 21 aeroplanes. The approval of aeroplanes in accordance with Part 21 is ratified by the issue of a Type Certificate (TC) or Restricted TC (RTC) by the CAA. In general, there will be a Type Certificate Data Sheet (TCDS) associated with each TC or RTC issued. The TCDS records the basis of certification, the designation BD-100-1A10 Challenger 300 and Challenger 350 CL-30 Approved by the Aircraft Evaluation Division Federal Aviation Administration Transport Aircraft Long Beach Aircraft Evaluation Group 3960 Paramount Boulevard, Suite 100 Lakewood, CA 90712 -4137 Office Telephone: (562) 627-5317 Office Fax: (562) 627-5210 BD-100-1A10 Date: Apr 16/12 REV-1 RECORD OF REVISIONS Retain this index in the front of the manual. When Revisions are received and inserted, enter the relevant information in the columns below. Revision # Pages Affected By Original All Rev. 1 TOC-1, Manual Approval Page, REV-1, HOC-1,23-1,25-1,28-1,31-1,34-5,34-6 Rev. 2 All 5.2.8 Time intervals for cleaning drain pipes or culverts 5.2.9 Oil and fuel separators 5.2.10 Cleaning the oil and fuel separators 5.2.11 Cleaning the bottom and banks of the drain water collector basins 5.2.12 Removal of oil and fuel from separators 5.3 Water Hydrants 5.3.1 Airport's water supply system 5.3.2 Airport Fire hydrants Chapter 6. Technical Specification of BVL Boeing 737-300 Winglets 3. LOPA 4. Exterior of BVL Boeing 737-300 Winglets 5. Interior of BVL Boeing 737-300 Winglets . Aircraft statuses - as of Apr 2019 Model Serial Number Variable Tab Number Line Number Date of Manufacture TSN CSN AIRCRAFT 737-33S 29072 PRIOI 3012 31.03.1998 Certification Specifications for Operational Suitability Data (OSD) Flight Crew Data CS-FCD Initial Issue (Book 1), dated 31st January 2014 8. Environmental Standards: Noise BD-700-1A10 aircraft), or BA Service Bulletin 700-1A11-34-005 (for BD-700-1A11 aircraft), in that it has 5 Maximum Permissible Take−Off Weight (Wat Limit) − Flaps 15 Degrees 6 Take−Off Runway Length Requirements − Flaps 5 Degrees 7 Take−Off Runway Length Requirements − Flaps 10 Degrees 8 Take−Off Runway Length Requirements − Flaps 15 Degrees 9 Max. Landing Weight − Landing Flaps 10 and Approach Flaps 5 Degrees 10 Max. Operations Specifications 5 Luftfahrzeugmuster 5 Aircraft Model BD-700-1A 10 6 25. September 2013 30. September 2015 Boeing 737-800 1 25. Februar 2014 30. September 2015 Cessna Model 750 (Citation X) 2 25. September 2013 30. September 2015 Falcon 2000EX 3 Rev. 1 08. Oktober 2013 30. September 2015 Falcon