Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 367
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DA 42 NG AFM Airplane Description
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 19
7.6 SEATS AND SAFETY HARNESSES
To increase passive safety, the seats are constructed using a carbon fiber/Kevlar hybrid
material and GFRP. The seats are removable to allow maintenance and inspection of
the underlying controls. Covers on the control sticks prevent loose objects from falling
into the area of the controls.
The seats have removable furnishings and are equipped with energy-absorbing foam
elements.
The seats are fitted with three-part safety harnesses. The harnesses are fastened by
inserting the end of the belts in the belt lock, and are opened by pressing the red release
on the belt lock.
The backs of the rear seats can be laid forward after pulling upwards on the locking bolt
knob.
If front seats with adjustable backrests are installed (OÄM 42-067), the angle of the
backrests can be adjusted for best comfort. The backrest lever is situated on the outboard
side of the backrest. However, during take-off, landing and emergency landing the
backrests must be fixed in the upright position designated by a placard on the roll-over
bar.
CAUTION
Before the backrest lever is lifted in order to unlock the
backrest, lean back towards the backrest to counteract the
spring load; otherwise the backrest may snap forward.
CAUTION
Do not apply a load of more than 900 N (202 lbf) to the top
of the backrest. Damage to the adjustment mechanism may
otherwise result.
- 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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