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Technify Motors TAE 125-02-114 Manual Supplement Download Page 62

AFM Supplement DA 40 D

Page 7-1

Issue 2

Revision -, Aug. 2015

CHAPTER 7

DESCRIPTION OF THE AIRPLANE AND 

ITS SYSTEMS

7.9.1 ENGINE, GENERAL

The TAE 125-02-114 engine has the same general characterics 
as the TAE 125-02-99 engine, except for the continuous and 
maximum power.

Max. power:

114 kW (155 DIN-HP) at 2300 RPM,  ISA, SL

Max. cont. power:114 kW (155 DIN-HP) at 2300 RPM,  ISA, SL

There is no difference in operation between the different TAE 
125 engine variants.

Summary of Contents for TAE 125-02-114

Page 1: ...EASA approved Airplane Flight Manual when the TAE 125 02 114 engine has been installed in accordance with EASA STC 10036328 The information contained in this supplement supersedes or adds to the EASA...

Page 2: ...This page intentionally left blank...

Page 3: ...ion No 1 to AFM supplement ref 50 0310 50021 is approved under the authority of DOA ref EASA 21J 010 Date March 16 2012 Office of Airworthiness 2 0 All Change of Ownership Aug 15 2015 EASA STC 1003632...

Page 4: ...the authority of EASA DOA No EASA 21J 010 in accordance with Part 21 GENERAL REMARK The content of this AFM supplement is developed on basis of the EASA approved AFM DAI Document No 6 01 05 E Chapter...

Page 5: ...apter CHAPTER 4a NORMAL OPERATING PROCEDURES a non approved chapter CHAPTER 4b ABNORMAL OPERATING PROCEDURES a non approved chapter CHAPTER 5 PERFORMANCE a non approved chapter CHAPTER 6 WEIGHT AND BA...

Page 6: ...AFM Supplement DA 40 D Page vi Issue 2 Revision Aug 2015 This page is intentionally left blank...

Page 7: ...rmation not contained in this supplement consult the basic EASA approved Airplane Flight Manual 1 2 CERTIFICATION BASIS The certification basis for the TAE 125 02 114 engine installation is CS 23 date...

Page 8: ...AFM Supplement DA 40 D Page 1 2 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 9: ...PM Max continuous power 114 kW 155 HP at 2300 RPM Max recommended cruise power 85 e Oil Pressure Min oil pressure 1 2 bar Min oil pressure at Take off power 2 3 bar Min oil pressure in flight 2 3 bar...

Page 10: ...ater Radiator Protection at a ratio of 50 50 Radiator Protection BASF Glysantin Protect Plus G48 Mobil Antifreeze Extra G48 ESSO Antifreeze Extra G48 Comma Xstream Green Concentrate G48 Zerex Glysanti...

Page 11: ...ermined and the problem must be corrected by authorized personnel Indi cation Red arc bar lower prohibited range Yellow arc bar caution range Green arc bar normal operating range Yellow arc bar cautio...

Page 12: ...N EN590 TS 1 GOST 10227 86 TS 1 GSTU 320 00149943 011 99 SASOL GTL Diesel Volt meter V below 11 11 to 12 5 12 6 to 14 9 15 0 to 15 5 above 15 5 Fuel qty US gal below 0 45 0 45 to 14 CAUTION Intentiona...

Page 13: ...ent DA 40 D Page 2 5 Issue 2 Revision Aug 2015 2 16 OTHER LIMITATIONS Fuel Temperature The fuel temperature limitations applicable for the TAE 125 02 99 engine are valid for the TAE 125 02 114 Refer t...

Page 14: ...3 1 Issue 2 Revision Aug 2015 CHAPTER 3 EMERGENCY PROCEDURES The emergency procedures included in this chapter supersede the procedures in the basic AFM For emergency procedures not included in this...

Page 15: ...IC MASTER ON 8 Airspeed 70 110 KIAS continued next page Note As long as an airspeed of at least 70 KIAS is maintained and there is no major mechanical engine defect the propeller will continue to wind...

Page 16: ...it is not possible to start the engine adopt glide configuration carry out emergency landing Refer to basic AFM CAUTION Engine restart following an engine fire should only be attempted if it is unlik...

Page 17: ...ir OPEN 6 Fuel transfer pump ON 7 AVIONIC MASTER OFF 8 ELECTRIC MASTER ON 9 ENGINE MASTER ON continued next page Note Restarting the engine with stationary propeller is possible at altitudes below 140...

Page 18: ...should be set to ON see 3 2 4 RESTARTING THE ENGINE WITH WINDMILLING PROPELLER of this supplement A loss of altitude of at least 1000 ft 300 meters must be expected If it is not possible to start the...

Page 19: ...AFM Supplement DA 40 D Page 3 6 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 20: ...he TAE 125 02 114 engine installation For normal operating procedures refer to basic AFM Flight Mass 980 kg 2160 lb 1000 kg 2205 lb 1150 kg 2535 lb Airspeed for rotation Take off run VR Flaps T O 54 K...

Page 21: ...AFM Supplement DA 40 D Page 4A 2 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 22: ...AFM Supplement DA 40 D Page 4B 1 Issue 2 Revision Aug 2015 CHAPTER 4B ABNORMAL OPERATING PROCEDURES For abnormal operating procedures refer to basic AFM...

Page 23: ...AFM Supplement DA 40 D Page 4B 2 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 24: ...LES AND DIAGRAMS 5 3 2 Diagram for setting engine performance Not valid for TAE 125 02 114 engine installation Note This chapter applies to aircraft with propeller MTV 6 A 187 129 The correct designat...

Page 25: ...ll Over 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m SL 316 510 340 551 366 594 393 639 1000 334 539 360 582 387 628 416 67...

Page 26: ...Ground Roll Over 50ft obstacle Ground Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft SL 1037 1673 1116 1808 1201 1949 1289 2097 1000 1096 1768 1181 1910 1270 2060 1365 2215 2000 1158 1870 1250 202...

Page 27: ...5m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m SL 220 355 237 383 255 413 274 444 1000 232 375 250 405 269 436 289 470 2000 24...

Page 28: ...bstacle Ground Roll Over 50ft obstacle Ground Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft SL 722 1165 778 1257 837 1355 899 1457 1000 761 1230 820 1329 883 1430 948 1542 2000 807 1303 869 1404...

Page 29: ...m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m SL 208 336 225 363 242 392 260 421 1000 220 356 237 384 256 414 274 446 2000 233...

Page 30: ...obstacle Ground Roll Over 50ft obstacle Ground Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft SL 682 1102 738 1191 794 1286 853 1381 1000 722 1168 778 1260 840 1358 899 1463 2000 764 1234 824 1332...

Page 31: ...Take off climb performance at 1150 kg 2535 lb Weight 1150 kg 2535 lb Flaps T O Airspeed for initial climb 66 KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 1...

Page 32: ...150 kg 2535 lb Flaps UP Airspeed for initial climb 78 KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F SL 815 785 754...

Page 33: ...UP Airspeed for initial climb 78 KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F SL 1023 989 955 921 1000 1018 983 94...

Page 34: ...UP Airspeed for initial climb 78 KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F SL 1055 1020 986 952 1000 1050 1015...

Page 35: ...standard tanks with 106 l 28 US gal usable fuel 2 Endurance time of this table is reduced by the time for startup and taxi time fuel and distance to climb and 45 min reserve 3 The range data of this t...

Page 36: ...365 2 7 2000 80 131 25 8 6 8 415 3 2 2000 70 124 22 1 5 8 473 3 8 2000 60 115 18 6 4 9 541 4 7 2000 50 105 15 3 4 0 617 5 8 4000 100 146 33 6 8 9 325 2 2 4000 90 140 29 6 7 8 367 2 6 4000 80 133 25 8...

Page 37: ...143 25 8 6 8 422 2 7 12000 70 134 22 1 5 8 477 3 3 12000 60 125 18 6 4 9 541 4 1 12000 50 113 15 3 4 0 611 5 1 14000 80 145 25 8 6 8 424 2 6 14000 70 137 22 1 5 8 478 3 2 14000 60 127 18 6 4 9 540 3 9...

Page 38: ...anks with 147 6 l 39 US gal usable fuel 2 Endurance time of this table is reduced by the time for startup and taxi time fuel and distance to climb and 45 min reserve 3 The range data of this table tak...

Page 39: ...8 558 4 1 2000 80 131 25 8 6 8 626 4 8 2000 70 124 22 1 5 8 706 5 7 2000 60 115 18 6 4 9 799 6 9 2000 50 105 15 3 4 0 903 8 6 4000 100 146 33 6 8 9 505 3 4 4000 90 140 29 6 7 8 563 4 0 4000 80 133 25...

Page 40: ...43 25 8 6 8 653 4 3 12000 70 134 22 1 5 8 730 5 2 12000 60 125 18 6 4 9 820 6 3 12000 50 113 15 3 4 0 918 7 8 14000 80 145 25 8 6 8 658 4 2 14000 70 137 22 1 5 8 735 5 1 14000 60 127 18 6 4 9 823 6 2...

Page 41: ...AFM Supplement DA 40 D Page 5 a 18 Issue 2 Revision Aug 2015 5 3 15 Approved Noise Data With TAE 125 02 114 engine and Muffler LA50 Installed ICAO Annex 16 Chapter X 69 6 dB A...

Page 42: ...LES AND DIAGRAMS 5 3 2 Diagram for setting engine performance Not valid for TAE 125 02 114 engine installation Note This chapter applies to aircraft with propeller MTV 6 A 190 69 The correct designati...

Page 43: ...d Roll Over 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m m m SL 275 458 294 488 314 522 343 571 362 605 1000 291 484 311 516 332 552 363 605 383 640 2000...

Page 44: ...Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft ft ft SL 903 1501 963 1601 1028 1711 1124 1874 1187 1984 1000 954 1587 1019 1694 1088 1810 1190 1984 1257 2101 2000 1009 1679 1078 1793 1152 1916 12...

Page 45: ...er 15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m m m SL 217 361 232 385 247 412 255 425 286 477 1000 230 382 245 408 262 436 269 449 303 506 2000 243 404...

Page 46: ...le Ground Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft ft ft SL 712 1185 760 1264 812 1350 835 1393 937 1566 1000 753 1253 804 1337 859 1429 884 1474 993 1658 2000 797 1325 851 1415 909 1513 936...

Page 47: ...15m obstacle Ground Roll Over 15m obstacle Ground Roll Over 15m obstacle ft m m m m m m m m m m SL 182 302 194 322 207 344 213 355 239 399 1000 192 319 205 341 219 364 225 376 253 422 2000 203 338 21...

Page 48: ...obstacle Ground Roll Over 50ft obstacle ft ft ft ft ft ft ft ft ft ft ft SL 595 990 635 1057 678 1129 698 1164 783 1309 1000 630 1047 672 1118 718 1194 739 1232 830 1386 2000 666 1108 711 1183 760 12...

Page 49: ...150 kg 2535 lb Weight 1150 kg 2535 lb Flaps T O Airspeed for initial climb 66 KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C...

Page 50: ...KIAS Power MAX Pres Alt RATE OF CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F ISA 35 C ISA 63 F SL 918 913 901 829 918 1000 914 909 896 824 914 200...

Page 51: ...CLIMB feet per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F ISA 35 C ISA 63 F SL 1048 1043 1030 952 888 1000 1044 1038 1026 947 884 2000 1039 1034 1021 942 879...

Page 52: ...t per minute Temperature C F ft ISA ISA 10 C ISA 18 F ISA 20 C ISA 36 F ISA 30 C ISA 54 F ISA 35 C ISA 63 F SL 1153 1148 1135 1051 984 1000 1149 1144 1131 1047 979 2000 1144 1140 1126 1042 975 3000 11...

Page 53: ...standard tanks with 106 l 28 US gal usable fuel 2 Endurance time of this table is reduced by the time for startup and taxi time fuel and distance to climb and 45 min reserve 3 The range data of this t...

Page 54: ...0 133 25 8 6 8 424 3 1 2000 70 126 22 1 5 8 485 3 8 2000 60 118 18 6 4 9 556 4 6 2000 50 109 15 3 4 0 639 5 8 4000 100 148 33 6 8 9 334 2 1 4000 90 142 29 6 7 8 378 2 5 4000 80 136 25 8 6 8 428 3 0 40...

Page 55: ...146 25 8 6 8 446 2 7 12000 70 138 22 1 5 8 507 3 3 12000 60 129 18 6 4 9 577 4 1 12000 50 117 15 3 4 0 654 5 2 14000 80 149 25 8 6 8 450 2 6 14000 70 141 22 1 5 8 512 3 2 14000 60 131 18 6 4 9 582 4 0...

Page 56: ...anks with 147 6 l 39 US gal usable fuel 2 Endurance time of this table is reduced by the time for startup and taxi time fuel and distance to climb and 45 min reserve 3 The range data of this table tak...

Page 57: ...8 25 8 639 4 7 2000 70 126 22 1 22 1 723 5 7 2000 60 118 18 6 18 6 821 6 9 2000 50 109 15 3 15 3 935 8 5 4000 100 148 33 6 33 6 517 3 4 4000 90 142 29 6 29 6 577 3 9 4000 80 136 25 8 25 8 647 4 6 400...

Page 58: ...25 8 25 8 681 4 3 12000 70 138 22 1 22 1 767 5 2 12000 60 129 18 6 18 6 866 6 3 12000 50 117 15 3 15 3 972 7 9 14000 80 149 25 8 25 8 691 4 2 14000 70 141 22 1 22 1 777 5 1 14000 60 131 18 6 18 6 874...

Page 59: ...AFM Supplement DA 40 D Page 5 b 18 Issue 2 Revision Aug 2015 5 3 15 Approved Noise Data With TAE 125 02 114 engine and Muffler LA50 Installed ICAO Annex 16 Chapter X 70 5 dB A...

Page 60: ...E EQUIPMENT LIST 6 3 MASS AND BALANCE REPORT After installation of the TAE 125 02 114 engine installation the empty mass and empty mass moment must be established Refer to the basic AFM and basic AMM...

Page 61: ...Motors GmbH ECU Firmware TAE 125 mx xx 02 7610 55101Rxx n a Mapping P14CxxxDA40 Clutch n a Mapping P14DxxxDA40 Dual Mass Fly Wheel ECU D4 05 7611 E0019 04 Technify Motors GmbH ECU Firmware D4 vx xx 05...

Page 62: ...E GENERAL The TAE 125 02 114 engine has the same general characterics as the TAE 125 02 99 engine except for the continuous and maximum power Max power 114 kW 155 DIN HP at 2300 RPM ISA SL Max cont po...

Page 63: ...1 for a schematic Figure 7 1 Liquid Cooling System 7 9 8 OIL SYSTEMS Lubrication system engine and turbocharger The engine oil is cooled using a oil water heat exchange which is part of the engine Th...

Page 64: ...It supersedes or adds to the basic DAI Airplane Maintenance Manual only as set forth therein 8 2 AIRPLANE INSPECTION INTERVALS Refer to supplement to the Airplane Maintenance Manual AMM 50 02 and the...

Page 65: ...AFM Supplement DA 40 D Page 8 2 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 66: ...AFM that are affected by the TAE 125 02 114 engine istallation For the affected supplements a supplement has been created which adds or supersedes the affected supplements as described 9 2 LIST OF SUP...

Page 67: ...AFM Supplement DA 40 D Page 9 2 Issue 2 Revision Aug 2015 This page intentionally left blank...

Page 68: ...ne Flight Manual when the TAE 125 02 114 engine has been installed in accordance with EASA STC 10036328 The information contained in this supplement supersedes or adds to the EASA approved Airplane Fl...

Page 69: ...e 9 1 2 Issue 2 Revision Aug 2015 Issue Pages Description Approved Date Endorsed 2 0 All New Issue Change of Ownership Aug 15 2015 EASA STC 10036328 Rev 3 Remark The parts of the text which changed ar...

Page 70: ...2 114 engine installation 2 Limitations No change The engine limitations and engine instrument marking applicable to the TAE 125 02 99 engine are valid for the TAE 125 02 114 Refer to supplement A31 o...

Page 71: ...min G1000 VFR Page 9 1 4 Issue 2 Revision Aug 2015 7 Description of the airplane and its systems No change Refer to supplement A31 of the basic AFM 8 Airplane Handling Care and Maintenance No change R...

Page 72: ...ne Flight Manual when the TAE 125 02 114 engine has been installed in accordance with EASA STC 10036328 The information contained in this supplement supersedes or adds to the EASA approved Airplane Fl...

Page 73: ...e 9 2 2 Issue 2 Revision Aug 2015 Issue Pages Description Approved Date Endorsed 2 0 All New Issue Change of Ownership Aug 15 2015 EASA STC 10036328 Rev 3 Remark The parts of the text which changed ar...

Page 74: ...2 114 engine installation 2 Limitations No change The engine limitations and engine instrument marking applicable to the TAE 125 02 99 engine are valid for the TAE 125 02 114 Refer to supplement A32 o...

Page 75: ...min G1000 IFR Page 9 2 4 Issue 2 Revision Aug 2015 7 Description of the airplane and its systems No change Refer to supplement A32 of the basic AFM 8 Airplane Handling Care and Maintenance No change R...

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