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AFM Supplement DA 40 D

Page 5(a)-8
Issue 2
Revision -, Aug. 2015

5.3.8 Climb Performance - Take-off climb

Take-off at 1150 kg, 2535 lb

Notes:
1.

For operation in air colder than provided, use coldest data

2.

For operation in air warmer than provided, use extreme caution 

Table 5(a)-7 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+18°F

ISA+20°C

ISA+36°F

ISA+30°C

ISA+54°F

SL

646

630

614

598

1000

645

629

613

597

2000

643

627

612

596

3000

642

626

610

594

4000

641

625

609

593

5000

640

624

608

592

6000

638

622

606

590

7000

637

621

605

589

8000

636

619

603

587

9000

614

598

582

567

10000

587

572

557

541

Содержание TAE 125-02-114

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

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

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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