Appendix G to Part 135 - Design-Life GoalsAppendix 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 ---------------------------------------------------------------------------------------------------------------- Effective Date Note: At 67 FR 72766, Dec. 6, 2002, Appendix G to
part 135 was added, effective Dec. 8, 2003.
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