Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 340
- Page / 440
- Table of contents
- BOOKMARKS
Rated. / 5. Based on customer reviews
DA 42 NG AFM Mass and Balance
Airplane Serial No.: Registration: Date: Mass Lever Arm
Description Type Part No. Manufacturer S/N installed lb kg in m
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 26
Headset, pilot Echelon 100 Telex
Headset, pilot HMEC25-KAP-2 025-230-715 Sennheiser
Headset, co-pilot Echelon 100 Telex
Headset, co-pilot HMEC25-KAP-2 025-230-715 Sennheiser
Headset, LH pax Echelon 100 Telex
Headset, LH pax HMEC25-KAP-2 025-230-715 Sennheiser
Headset, RH pax Echelon 100 Telex
Headset, RH pax HMEC25-KAP-2 025-230-715 Sennheiser
Speaker FRS8 / 4 Ohms Visaton
Handmic 100 TRA 62800-001 Telex
Pitot / Static probe, heated AN5814-2 PST-305 Aeroinstruments
Alternate static valve DA4-3111-51-00 Diamond Aircraft
Backup altimeter 5934PD-3 United Instruments 0.496 0.225 70.080 1.780
Backup altimeter LUN 1120 1120.23B2X Mikrotechna
Backup airspeed indicator 8030 8030-B.879 United Instruments 0.680 0.308 70.080 1.780
Backup airspeed indicator
% 8030% 8030-B.910% United Instruments%
%%
0.680% 0.308% 70.080% 1.780%
Backup artificial horizon 4300 4300-206 Mid Continent Instr. 2.500 1.134 70.080 1.780
Magnetic compass PG2C-28V SIRS Navigation
OAT probe GTP 59 011-00978-00 Garmin
Digital air data system GDC74A 011-00882-00 Garmin 1.690 0.770 70.080 1.780
Digital air data system GDC 74A 011-00882-10 Garmin 1.690 0.770 70.080 1.780
Integrated avionics #1 GIA 63 W 011-01105-20 Garmin 5.290 2.400 154.900 3.935
Integrated avionics #2 GIA 63 W 011-01105-20 Garmin 5.290 2.400 154.900 3.935
Integrated avionics #1 GIA 63W 011-01105-01 Garmin 5.290 2.400 154.900 3.935
Integrated avionics #2 GIA 63W 011-01105-01 Garmin 5.290 2.400 154.900 3.935
Transponder GTX 33 011-00779-10 Garmin 3.100 1.410 153.100 3.890
- Intentionally left blank 2
- 0.1 APPROVAL 4
- 0.2 RECORD OF REVISIONS 4
- 0.3 LIST OF EFFECTIVE PAGES 6
- Introduction DA 42 NG AFM 10
- Ch. Page Date 10
- DA 42 NG AFM Introduction 11
- 0.4 TABLE OF CONTENTS 16
- CHAPTER 1 17
- 1.1 INTRODUCTION 18
- 1.2 CERTIFICATION BASIS 21
- 1.4 DIMENSIONS 22
- 1.6 UNITS OF MEASUREMENT 33
- 1.7 THREE-VIEW DRAWING 36
- 1.8 G1000 AVIONICS SYSTEM 37
- 1.9 SOURCE DOCUMENTATION 39
- CHAPTER 2 41
- OPERATING LIMITATIONS 41
- 2.1 INTRODUCTION 43
- NOTE' 43
- 2.2 AIRSPEED 44
- 2.4 POWER-PLANT LIMITATIONS 46
- 2.7 MASS (WEIGHT) 57
- 2.8 CENTER OF GRAVITY 59
- 2.9 APPROVED MANEUVERS 61
- 2.10 MANEUVERING LOAD FACTORS 62
- 2.11 OPERATING ALTITUDE 63
- 2.12 FLIGHT CREW 63
- 2.13 KINDS OF OPERATION 63
- 2.14 FUEL 67
- CAUTION' 68
- 2.15 LIMITATION PLACARDS 70
- LANDING GEAR 71
- EMERGENCY 71
- Gear Extension 71
- Max. 152 KIAS 71
- APPROVED FUEL 72
- 133 KIAS 73
- 113 KIAS 73
- 2.16 OTHER LIMITATIONS 76
- CHAPTER 3 85
- EMERGENCY PROCEDURES 85
- 3.1 INTRODUCTION 88
- 3.4 G1000 SYSTEM WARNINGS 100
- 3.5 G1000 FAILURES 102
- 3.6 ABNORMAL ENGINE BEHAVIOUR 106
- 3.8 ENGINES OUT LANDING 129
- 3.11 SMOKE AND FIRE 141
- 3.12 OTHER EMERGENCIES 146
- CHAPTER 4A 159
- NORMAL OPERATING PROCEDURES 159
- 4A.1 INTRODUCTION 161
- 4A.4 FLIGHT CHARACTERISTICS 164
- 4A.5 DAILY CHECK 164
- Fuel Quantity% 222
- Fuel Additive BIOBOR JF*% 222
- 135 ppm% 270 ppm% 222
- ** Do not batch blend% 223
- CAUTION 224
- CONTINUED 226
- Normal Operating 228
- Procedures 228
- DA 42 NG AFM 228
- CHAPTER 4B 229
- ABNORMAL OPERATING PROCEDURES 229
- 4B.1 PRECAUTIONARY LANDING 231
- RANGE ON THE G1000 234
- 4B.9 LIGHTNING STRIKE 262
- INSTALLED) 270
- CHAPTER 5 271
- PERFORMANCE 271
- 5.1 INTRODUCTION 272
- DA 42 NG AFM Performance 275
- Performance DA 42 NG AFM 282
- 1000' 282
- 00' 284
- Gradient 287
- Go-Around Climb Performance 313
- CHAPTER 6 315
- MASS AND BALANCE 315
- 6.1 INTRODUCTION 316
- 6.3 MASS AND BALANCE REPORT 318
- Mass and Balance DA 42 NG AFM 324
- 6.4.2 LOADING DIAGRAM 324
- DA 42 NG AFM Mass and Balance 325
- Flight Mass [kg] 330
- Center of Gravity Positio 330
- Flight Mass [lb] 332
- Flight Mass Moment [kg m] 332
- Flight Mass Moment [in lb] 332
- % 0.308% 70.080% 1.780% 340
- % mt-propeller 344
- CHAPTER 7 349
- DESCRIPTION OF THE AIRPLANE 349
- AND ITS SYSTEMS 349
- 7.1 INTRODUCTION 351
- 7.2 AIRFRAME 351
- 7.3 FLIGHT CONTROLS 352
- 7.4 INSTRUMENT PANEL 359
- 7.5 LANDING GEAR 361
- 7.7 BAGGAGE COMPARTMENT 369
- Floor Panel 372
- Emergency Axe 372
- 7.9 POWER PLANT 373
- 7.9.5 FUEL SYSTEM 383
- 7.10 ELECTRICAL SYSTEM 397
- ADVISORY 406
- 7.11 PITOT-STATIC SYSTEM 412
- 7.12 STALL WARNING SYSTEM 412
- 7.14 AVIONICS 418
- CHAPTER 8 425
- 8.1 INTRODUCTION 426
- Handling, Care 432
- Maintenance 432
- 8.6 CLEANING AND CARE 434
- 8.7 GROUND DE-ICING 436
- CHAPTER 9 437
- SUPPLEMENTS 437
- 9.1 INTRODUCTION 438
- 9.2 LIST OF SUPPLEMENTS 439
- % 01-Apr-2014% 99 439
© 2020, manymanuals.com. All rights reserved. | 0.663 s |
Manymanuals.com
Manymanuals.de
Manymanuals.fr
Manymanuals.it
Manymanuals.pl
Manymanuals.cz
Manymanuals.es
Manymanuals-pt.com
Comments to this Manuals