EA 400 - Extra Aircraft

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Pilot’s Operating Handbook EA 400 Section 2 Limitations 2.6 Powerplant Instrument Markings Instrument Red Line Min. Limit Yellow Arc Green Arc Yellow Arc Caution Range Normal Operating Caution or Takeoff Red Line Max. Limit Tachometer, RPM 600-2,500 2,500-2,600 2,600 Manifold Pressure in. Hg. bar Exhaust Gas Temp. °C °F Cylinder Head Temp. °C °F Oil Temperature °C °F Oil Pressure bar PSI Coolant Temperature °C °F Fuel Pressure bar PSI Turbine Inlet Temp. °C °F 38 100 0.7 10 66 150 0.7-2.1 10-30 0-0.21 0-3 0-37.5 0-1.27 650-954 1200-1750 93-191 200-375 77-93 170-200 2.1-4.1 30-60 82-93 180-200 0.21-0.41 3-6 37.5-39.5 1.27-1.34 93-110 200-230 4.1-7 60-100 93-110 200-230 >0.41 >6 39.5 1.34 954 1750 191 375 110 230 7 100 110 230 954 1750 Vacuum Diff. Press. in. Hg 4.5 4.5-5.2 5.2 Issued: 15. 8. December October 1999 2000 2-7
Section 2 Limitations Pilot’s Operating Handbook EA 400 2.7 Miscellaneous Instrument Markings Instrument Red Line Min. Limit Yellow Arc Green Arc Yellow Arc Caution Range Normal Operating Caution or Takeoff Red Line Max. Limit Voltmeter, V 23 23-26 26-29 29-32 32 Cabin Altitude, ft 10,000 Cabin Differential Pressure, PSI 5.5 Fuel Quantity “0" -indication at 32 l (8.5 U.S. Gallons) unusable fuel each tank, red arc from 7 l (1.85 U.S. Gallons) to 32 l (8.5 U.S. Gallons) unusable 2.8 Weight Limits 1 Maximum Ramp Weight: 1999 kg (4407 lbs.) 2 Maximum Takeoff Weight: 1999 kg (4407 lbs.) 3 Maximum Landing Weight: 1999 kg (4407 lbs.) 4 Maximum Zero Fuel Weight: 1959 kg (4319 lbs.) 5 Maximum Empty Weight: 1555 kg (3428 lbs.) 6 Maximum Weight in Baggage Compartment: 90 kg (198 lbs.) 2.9 Center of Gravity Limits Values are given for landing gear extended configuration. 1 Aft Limit is defined at: 38 % of MAC 2 Forward Limit is defined by the following values: a 21 % of MAC at 1999 kg (4407 lbs.) (MTOW) b 12 % of MAC at 1600 kg (3527 lbs.) and below. C.G. range varies lineary between weight limits. MAC is 1322 mm (52.05 in.). 0% MAC is at 3200 mm. 2-8 Issued: 8. 15. December October 2000 1999
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Section 4 Normal Procedures Pilot
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Pilot’s Operating Handbook EA 400
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Section 8 Handling, Servicing and M
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Section 9 Supplements Pilot’s Ope
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Section 901 Pilot’s Operating Han
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Section 901 BENDIX/KING EFIS Pilot
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Section 901 BENDIX/KING EFIS a Pilo
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Section 903 BENDIX/KING KT 76A Pilo
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Section 903 BENDIX/KING KT 76A Pilo
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Section 904 BENDIX/KING EHSI/KI 256
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Section 905 BENDIX/KING KX 155 Pilo
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Section 906 BENDIX/KING KN 63 Pilot
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Section 907 BENDIX/KING KSG 105 wit
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Section 908 Handheld COM/NAV Icom I
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Section 909 BENDIX/KING KMA 24 Pilo
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Section 910 Intercom PS Engineering
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Section 911 Bose Headset Pilot’s
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Section 911 Bose Headset Pilot’s
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Section 912 SHADIN MINIFLO-L Pilot
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Section 912 SHADIN MINIFLO-L Pilot
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Section 913 POINTER 3000 ELT Pilot
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Section 913 POINTER 3000 ELT Pilot
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Section 914 Flashlight Pilot’s Op
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Section 915 GARMIN GNS 430 Pilot’
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Section 916 GARMIN GTX 320 Pilot’
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Section 917 GARMIN GMA 340 Pilot’
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Section 918 LITEF LCR-92 with CCU E
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Section 918 LITEF LCR-92 with CCU E
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Section 919 BENDIX/KING KDM 706A Pi
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Section 920 GARMIN GTX 327 FUNC Pil
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Section 921 Moritz Instrumentation
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Section 922 GARMIN GNS 530 NOTE Pil
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Section 925 Bendix/King KT 73 Pilot
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