Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 420
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Airplane Description DA 42 NG AFM
Page 7 - 72 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E
- Loss of the MFD will not cause the autopilot to disconnect, and will remain
engaged with limited functionality, but the autopilot cannot be re-engaged after
disconnect by the pilot.
- Loss of the PFD will cause the autopilot to disconnect. The autopilot and flight
director will be inoperative. Manual electric trim will be available.
- Loss of air data computer information will cause the autopilot to disconnect. The
autopilot will be inoperative. The flight director will be available except for air
data modes (ALT, VS, FLC). Manual electric trim is available.
- Loss of GIA #1 will cause the autopilot to disconnect. The autopilot, flight
director and manual electric trim will be inoperative. Loss of GIA #2 will also
prevent autopilot and manual electric trim operation, but flight director will be
available.
- Loss of the standby airspeed indicator, standby attitude indicator, standby
altimeter, or compass will have no effect on the autopilot.
- Loss of both GPS systems will cause the autopilot and flight director to operate
in NAV modes (LOC, BC, VOR, VAPP) with reduced accuracy. Course intercept
and station crossing performance may be improved by executing intercepts and
station crossings in HDG mode, then reselecting NAV mode.
The GFC 700 automatic flight control system (AFCS) installed in the Diamond DA 42 NG
consists of the following components:
- One GDU which contains the following mode control buttons:
AP (Autopilot engage/disengage)
FD (Flight director on/off)
HDG (Heading mode on/off)
NAV (Nav mode on/off)
APR (Approach mode on/off)
ALT (Altitude hold mode on/off)
- 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
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