[FAR 135, APPENDIX G: Design-Life Goals -- FAA FARS, 14 CFR] -- Flightsim Aviation Zone - Number 1 Flight Simulation and Aviation Resource! Information, Tools, Downloads, Databases, FAQ, Aviation Humour, Glossaries, Directory, FS2006, Multimedia, Screenshots, Free Flight Planner, Weather Reports | Aviation Databases - aircraft, airports, airlines, countries, timezones | Flight Simulator X
 
» Support this site -> Shop Online at Amazon!
Thursday 17 May 2012 03:56 GMT
 
 

FAA Federal Aviation Regulations (FARS, 14 CFR)

FARs   >   Part 135   >   Appendix G - Design-Life Goals

PREVIOUS Appendix F  |  Part 137 NEXT

FONT
serif sans
TEXT SIZE
T T T T
                                    Appendix G to Part  135._Design-Life Goals
------------------------------------------------------------------------------------------------------
Number of Design-life
Airplane type seats Type certificate data sheet goal (hours)
------------------------------------------------------------------------------------------------------
Raytheon (Beech) Aircraft Co.:
_Beech 99 (all models).................. 15+2 A14CE........................ 46,000
_Beech 1900 and 1900C................... 19+2 A24CE........................ 45,000
_Beech 300 and 300LW.................... 13+2 A24CE........................ 30,000
_Beech B300 and B300C................... 15+2 A24CE........................ 30,000
_Beech 1900D............................ 19+2 A24CE........................ 45,000
British Aerospace Ltd.:
_BAe Jetstream 3101..................... 19+2 A21EU........................ 45,000
_BAe Jetstream 3201..................... 19+2 A56EU........................ 30,000
Cessna Aircraft Co.:
_Cessna 402 Series (all models except 8+2 A7CE......................... 12,000
402C).
_Cessna 402C............................ 8+2 A7CE......................... 7,700
deHavilland Aircraft Co.:...................
_DHC-6.................................. 22+2 A9EA......................... 33,000
Dornier-Luftfahrt GmbH:
_Dornier 228-100 and -200............... 19+2 A16EU........................ 42,800
_Dornier 228-101 and -201............... 19+2 A16EU........................ 32,800
_Dornier 228-202........................ 19+2 A16EU........................ 29,600
_Dornier 228-212 (Except SN 155 & 19+2 A16EU........................ 26,400
191 and up).
_Dornier 228-212 (SN 155 and 191 and up) 19+2 A16EU........................ 42,800
Empresa Brasileira de Aeronautica (Embraer): 19+2 A21SO........................ 30,000
Embraer EMB-110.
Fairchild Aircraft Corporation:
_SA226-TC............................... 20+2 A8SW......................... 35,000
_SA227-AT............................... 14+2 A5SW......................... 35,000
_SA227-TT............................... 9+2 A5SW......................... 35,000
_SA227-AC............................... 20+2 A8SW......................... 35,000
_SA227-PC............................... 20+2 A8SW......................... 35,000
_SA227-BC............................... 20+2 A8SW......................... 35,000
_SA227-CC............................... 19+2 A18SW........................ 35,000
_SA227-DC............................... 19+2 A18SW........................ 35,000
Pilatus Britten-Norman: PBN BN-2 Mk III (all 16+2 A29EU........................ 20,480
models).
Piper Aircraft Inc., The New:
_PA 31 Navajo........................... 6+2 A20SO........................ 11,000
_PA 31-300 Navajo....................... 6+2 A20SO........................ 15,500
_PA 31P Pressurized Navajo.............. 6+2 A8EA......................... 14,000
_PA 31T Cheyenne and Cheyenne II........ 7+2 A8EA......................... 12,000
_PA 31-350 Chieftain and (T-1020)....... 9+2 A20SO........................ 13,000
_PA 31-325 Navajo CR.................... 9+2 A20SO........................ 11,000
_PA 31T2 Cheyenne II XL................. 5+2 A8EA......................... 11,400
_PA 31T3 (T-1040) without tip tanks..... 9+2 A8EA......................... 17,400
_PA 31T3 (T-1040) with tip tanks........ 9+2 A8EA......................... 13,800
Short Brothers PLC:.........................
_SD3-30................................. 39+2 A41EU........................ 57,600
_SD3-60................................. 39+2 A41EU........................ 28,800
_SD3-Sherpa............................. 39+2 A41EU........................ 40,000
------------------------------------------------------------------------------------------------------
PRINTABLE VERSION of this PageE-MAIL THIS PAGE to Somebody!SAVE TO FAVORITES / Bookmark this PageLINK TO THIS PAGE! (view simple HTML code)

Current page:   FARs   >   Part 135   >   Appendix G - Design-Life Goals

PREVIOUS Appendix F  |  Part 137 NEXT

page stats: viewed 876 unique times - last change 26-Feb-2005

SEARCH the FARS :

Top of Page

» DOWNLOADING (PARTS OF) THIS WEBSITE AUTOMATICALLY IS NOT ALLOWED! «

THIS IS NO OFFICIAL SOURCE -- [DISCLAIMER] [FAA WEBSITE]

See also: AIM | ATC | FSS | NOTAMS | PCG |

 
Top of page
add to favorites @ E-mail this! Link to this!
Top of page
© 2002-2012 - Legal | Contact | Advertise | Sitemap
Visit our $pons0rs:
Your site here?
hosted by 123XS || also visit: Flightsim Search & Aviation Search || Link to us!