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EFTA01194929

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A`- 1-4 GIV/G300/G400 PILOT TRAINING MANUAL 38' 1-14" 20 FT RADIUS NOTE: CONDITIONS-AIRCRAFT STATIC, SEA LEVEL ISA NO WIND 77' 10" 32, 0.. 41,,60:3 NOTE: AIRCRAFT WITH SATCOM ANTENNA ON TOP OF THE 13' 8" VERTICAL FIN HAVE A HEIGHT IN EXCESS OF 24' 5-1/8" 88' 4" Figure 1-3. General Dimensions Figure 1-4. MAX RPM TEMPERATURE DROPS TO 30°C 351 FT 200 FT FUS Gen The f divide trance ment a fusela wing, the no≤ the for' aft of tl inches wheel senger N In addi compar 24' 5-1/8" which APU, a 1 MAX RPM VELOCITY DROPS TO 20 MPH 70 FT 400 FT LEGEND AREA TO BE CLEARED OF PERSONNEL BEFORE ENGINE START OR DURING IDLE ADDITIONAL AREA TO BE CLEARED OF PERSONNEL BEFORE OPERATING AT MAXIMUM THRUST Engine Operating Danger Areas FOR TRAINING Pumpr,-- NOSE ( EFTA01194929

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Independent research project. Not affiliated with the U.S. Department of Justice, FBI, any government agency, or Anthropic. All analytical text on this site is AI-generated (Claude, Anthropic) and iteratively fact-checked against source documents, but may contain errors. Verify all claims against linked EFTA sources before citing.
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