Earth alerts 2017 1 42

N) Propeller manufacturer : mt-Propeller o) Propeller designation : MTV-6-A-C-F/CF 187-129... Page 44 Operating Limitations DA 42 AFM CAUTION If the coolant or gearbox oil level is low, the reason must be determined and the problem must be corrected by authorized personnel. v) Maximum restart altitude 6000 ft w) Restart airspeed 80 to 120 KIAS Page 2 - 8 Rev. Page 45: Engine Instrument Markings DA 42 AFM Operating Limitations 2.5 ENGINE INSTRUMENT MARKINGS Engine instrument markings and their color code significance are shown in the table below: Indi- Yellow Green Yellow cation arc/bar arc/bar arc/bar arc/bar arc/bar lower caution normal caution upper prohibited range... Page 46: Warning, Caution And Advisory Alerts Operating Limitations DA 42 AFM 2.6 WARNING, CAUTION AND ADVISORY ALERTS 2.6.1 WARNING, CAUTION AND ADVISORY ALERTS ON THE G1000 NOTE The alerts described in the following are displayed on the Garmin G1000. Section 7.10 includes a detailed description of the alerts. Page 47 DA 42 AFM Operating Limitations Warning alerts Meaning / Cause (red) L/R ENG FIRE Left / Right engine fire detected. L/R STARTER Left / Right engine starter is engaged. DOOR OPEN Front and/or rear canopy and/or baggage door are/is not closed and locked. Page 48 Operating Limitations DA 42 AFM Color and significance of the caution alerts on the G1000 Caution-alerts Meaning / Cause (amber) * A fault has occurred in the left / right engine ECU A (one reset of minor faults is possible) Page 49: Other Warning Alerts DA 42 AFM Operating Limitations Color and significance of the advisory alerts on the G1000 advisory alerts Meaning / Cause (white) L/R GLOW ON Left / Right engine glow plug active. L/R FUEL XFER Fuel transfer from auxiliary to main tank is in progress. Page 50: Mass (Weight) Operating Limitations DA 42 AFM 2.7 MASS (WEIGHT) Value Mass (Weight) Minimum flight mass 1250 kg 2756 lb Maximum take-off mass MÄM 42-088 not carried out 1700 kg 3748 lb MÄM 42-088 carried out 1785 kg 3935 lb Maximum zero fuel mass... Page 51: Center Of Gravity DA 42 AFM Operating Limitations 2.8 CENTER OF GRAVITY Datum Plane The Datum Plane (DP) is a plane which is normal to the airplane’s longitudinal axis and in front of the airplane as seen from the direction of flight. The airplane’s longitudinal axis is parallel with the floor of the nose baggage compartment. Page 52: Approved Maneuvers Operating Limitations DA 42 AFM 2.9 APPROVED MANEUVERS The airplane is certified in the Normal Category in accordance with JAR-23. Approved maneuvers 1) all normal flight maneuvers; 2) stalling (with the exception of dynamic stalling); and 3) Lazy Eights, Chandelles, as well as steep turns and similar maneuvers, in which an angle

Of the Earth’s and Mars’s figure,” Geodinamika, No. 2, 38–42 (2012). Google Scholar R. Blakey, Global Paleogeography. C. Maloof, G. P. Halverson, J. L. Kirschvink, et al., “Combined paleomagnetic, isotopic, and stratigraphic evidence for true polar wander from the Neoproterozoic Akademikerbreen Group, Svalbard, Norway,” Geol. Soc. Am. Bull. 118, 1099–1124 (2006).Article ADS Google Scholar National Centers for Environmental Information, ETOPO1 Global Relief Model. mgg/global/global.html.Scripps Orbit and Permanent Array Center Database. Wu, X. Collilieux, Z. Altamimi, et al., “Accuracy of the International Terrestrial Reference Frame origin and Earth expansion,” Geophys. Res. Lett. 38 (13), 124–129 (2011).Article Google Scholar Download referencesAuthor informationAuthors and AffiliationsLviv Polytechnic National University, Lviv, 79013, UkraineA. L. Tserklevych, O. S. Zayats & Ye. O. ShyloAuthorsA. L. TserklevychYou can also search for this author inPubMed Google ScholarO. S. ZayatsYou can also search for this author inPubMed Google ScholarYe. O. ShyloYou can also search for this author inPubMed Google ScholarAdditional informationPublished in Ukrainian in Kinematika i Fizika Nebesnykh Tel, 2017, Vol. 33, No. 3, pp. 54–69.The article was translated by the authorsAbout this articleCite this articleTserklevych, A.L., Zayats, O.S. & Shylo, Y.O. Dynamics of the Earth shape transformation. Kinemat. Phys. Celest. Bodies 33, 130–141 (2017). citationReceived: 07 July 2016Published: 02 July 2017Issue Date: May 2017DOI:

Stopped: 6. Rudder ......neutral 7. Page 124 Emergency DA 42 AFM Procedures 3.9.7 EMERGENCY DESCENT 1. FLAPS ......UP 2. Page 125 Normal Operating DA 42 AFM Procedures CHAPTER 4A NORMAL OPERATING PROCEDURES Page 4A.1 INTRODUCTION ........4A-3 4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES . Page 126 Normal Operating DA 42 AFM Procedures 4A.6.14 SHUT-DOWN ....... . 4A-37 4A.6.15 PARKING . Page 127: Introduction Normal Operating DA 42 AFM Procedures 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... Page 128 NOTE is always less than v . For the DA 42 however, the actual value of v would be below the minimum safe speed. The minimum airspeed for best angle of climb was therefore raised... Page 129: Advisory Alerts On The G1000 Normal Operating DA 42 AFM Procedures 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 White color coded text CHARACTERISTICS 4A.3.2 L/R GLOW ON L/R GLOW ON Left / Right engine glow plug active 4A.3.3 L/R FUEL XFER... Page 130: Flight Characteristics Procedures 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. With the landing gear extended and at aft CG-locations, with flaps up and full power... Page 131: Daily Check Normal Operating DA 42 AFM Procedures 4A.5 DAILY CHECK Before the first flight of a day it must be ensured that the following functions are operable without failure. * On-condition check of the canopy, the side door and the baggage compartment doors for cracks and major scratches. Page 132 Normal Operating DA 42 AFM Procedures Center console: FUEL SELECTOR ..... check ON POWER Lever ......check condition, freedom of... Page 133 Normal Operating DA 42 AFM Procedures Check procedure: a) ELECT. MASTER ..... ON CAUTION When switching the ELECT. MASTER ON, the electrically driven hydraulic gear pump may activate itself for 5 to 20 seconds in order to restore the system pressure. Page 134 Normal Operating DA 42 AFM Procedures g) Control stick ......pull fully aft / hold at backstop h) FLAPS . Page 135 Normal Operating DA 42 AFM Procedures II. Walk-around check, visual inspection CAUTION A visual inspection means: examination for damage, cracks, delamination, excessive play, load transmission, correct attachment and general condition. In addition control surfaces should be checked for freedom of movement. Page 136 Normal Operating DA 42 AFM Procedures 2. Left engine nacelle: