European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA
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TCDS IM.A.070 Page 39/49<br />
Issue 04, 16 December 2010<br />
III. Technical Characteristics and Operational Limitations<br />
The GV is an airplane with two aft mounted turbofan engines, low swept wings with winglets,<br />
and a T-tail.<br />
1. <strong>EASA</strong>/JAA Type Design Definition<br />
Report GV-GER-1357, JAA GV Baseline Build Standard.<br />
Report GV-GER-6602, JAA Post Type Certification Modifications.<br />
<strong>EASA</strong>/JAA GV Certification is restricted to Aircraft Serial Number 541 and Subsequent.<br />
[Reference; JAA Certification Review Item (CRI) C-5 Issue 4, 25 September 2002]<br />
2. Engines<br />
Two Rolls Royce Deutschland BR700-710A turbofan engines.<br />
2.1 Engine Limits<br />
3. Fuel<br />
<strong>DATA</strong> SHEET: E00057EN (FAA)<br />
6305 (LBA) E.018 (<strong>EASA</strong>)<br />
Static thrust at sea level:<br />
� takeoff (5 minutes)*<br />
� maximum continuous<br />
65,611 N (14,750 lbs)<br />
64,277 N (14,450 lbs)<br />
* 10 minutes at take-off thrust allowed only in case of an inoperative engine due to<br />
shutdown or failure.<br />
Other engine limitations: See the Engine Type Certification Data Sheet.<br />
Kerosene<br />
American ASTM D 1655-92, Jet A<br />
ASTM D 1655-92, Jet A-1<br />
MIL-T-83133, Grade JP-8<br />
Canadian CAN/CGSB-3.23<br />
British DERD 2453<br />
DERD 2494<br />
French AIR 3405<br />
CIS GOST 10227-86, Am 1, TS-1 & RT<br />
IATA kerosene type<br />
Fuel shall conform to the specification as listed or to subsequent revisions found in the latest<br />
approved Airplane Flight Manual.
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