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4A.6.15 EXIT AIRPLANE .............................. 4A-40
4A.6.16 POST FLIGHT INSPECTION .................... 4A-40
4A.6.17 PARKING ................................... 4A-40
4A.6.18 FLIGHT IN RAIN .............................. 4A-41
4A.6.19 REFUELING ................................. 4A-41
4A.6.20 FLIGHT AT HIGH ALTITUDE .................... 4A-42
Page 4A - 2 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
4A.1 INTRODUCTION
Chapter 4A contains checklists and describes procedures for the normal operation of the airplane.
NOTE
Readability of the G1000 PFD and MFD displays may be degraded when wearing polarized sunglasses.
4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES
FLAPS up to 1700 kg above 1700 kg1 (above 3748 lb)
Airspeed for rotation (take-off run, vR) UP min. 70 KIAS min. 72 KIAS
Airspeed for take-off climb(best rate-of-climb speed vY) UP min. 77 KIAS min. 79 KIAS
Airspeed for best angle of climb2 UP 77 KIAS 79 KIAS
Airspeed for cruise climb UP min. 85 KIAS min. 86 KIAS
Reference landing approach speed UP 85 KIAS 86 KIAS
APP min. 82 KIAS 82 KIAS
Final approach speed LDG min. 76 KIAS min. 78 KIAS
Minimum speed during go around UP min. 82 KIAS min. 82 KIAS
Max. structural cruising speed Do not exceed this speed except insmooth air, and then only withcaution. UP 155 KIAS 155 KIAS
1), 2)
see NOTES on next page
NOTE
If M.M 42-088 is carried out, a landing with a mass between 1700 kg (3748 lb) and 1785 kg (3935 lb) is admissible. It constitutes an abnormal operating procedure. A "Hard Landing Check" is only required after a hard landing, regardless of the actual landing mass.
NOTE
vx is always less than vy. For the DA 42 however, the actual value of vx would be below the minimum safe speed. The minimum airspeed for best angle of climb was therefore raised to the value of vy.
Page 4A - 4 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
4A.3 ADVISORY ALERTS ON THE G1000
The G1000 provides the following advisory-alerts on the PFD in the alert area:
4A.3.1 ADVISORY/GENERAL
4A.3.2 L/R GLOW ON
4A.3.3 L/R FUEL XFER
4A.3.4 PFD/MFD/GIA FAN FAIL
PFD FAN FAIL Cooling Fan for the PFD is inoperative
MFD FAN FAIL Cooling Fan for the MFD is inoperative
GIA FAN FAIL Cooling Fan for the GIA is inoperative
The flight may be continued, but maintenance action is required after landing.
4A.4 FLIGHT CHARACTERISTICS
The DA 42 is to be flown with "the feet on the pedals“, meaning that coordinated flight in all phases and configurations shall be supported by dedicated use of the rudder and ailerons together.
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