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G7 Continuing airworthiness -
maintenance information ..............
SUB-PART H . Systems software .............
SUB-PART I . Crashworthiness and
cabin safety ................................
1.1 General ............................
1.2 Design emergency landing loads .......
1.3 Cabin fire protection .................
1.4 Evacuation .........................
1.5 Lighting and marking ................
1.6 Survival equipment ..................
SUB-PART J . Operating environment and
Human Factors .............................
J.1 General ............................
J.2 Flight crew .........................
J.3 Ergonomics ........................
J.4 Operating environmental factors ........
SUB-PART K . Security .....................
K.l Aeroplanes used for domestic
commercial operations ...............
K.2 Least-risk bomb location ....... ; ......
K.3 Protection of the flight crew
compartment .......................
K.4 Interior design ......................
PART IV. HELICOPTERS ..................
PART NA . Helicopters for which application for
certification was submitted on or after
22 March 1991 but before 13 December 2007 ....
CHAPTER 1. General ......................
1.1 Applicability .......................
IIIB-F-1
IIIB-F-1
IIIB-F- 1
IIIB-F-1
IIIB-F- 1
IIIB-F-2
IIIB-F-2
IIIB-G- 1
IIIB-G-1
IIIB-G-1
IIIB-G-1
IIIB-G-2
IIIB-G-2
IIlB-G-2
IIIB-H- 1
IIIB-1-1
IIIB-1-1
IIIB-1-1
IIIB-I- 1
IIIB-I- 1
IIIB-1-1
IIIB-I- 1
IIIB-K- 1
IIIB-K- 1
IIIB-K-1
IVA- 1.1
IVA- 1.1
IVA-1-1
Table of Contents Annex 8 -Airworthiness of Aircraj?
1.2 Limitations .........................
1.3 Unsafe features and characteristics ......
1.4 Proof of compliance ..................
CHAPTER 2 . Flight ........................
2.1 General ............................
2.2 Performance ........................
2.3 Flying qualities ......................
CHAPTER 3 . Structures .....................
3.1 General ............................
3.2 Airspeeds ...........................
3.3 Main rotor(s) rotational speed limits .....
3.4 Flight loads .........................
3.5 Ground and water loads ...............
3.6 Miscellaneous loads ..................
3.7 Flutter, divergence and vibration ........
3.8 Fatigue strength .....................
CHAPTER 4 . Design and construction .........
4.1 General ............................
CHAPTER 5 . Engines .......................
5.1 Scope ..............................
5.2 Design. construction and functioning ....
5.3 Declared ratings, conditions and
limitations ..........................
5.4 Tests ..............................
CHAPTER 6 . Rotor and power transmission
systems and powerplant installation .............
6.1 General ............................
6.2 Design, construction and functioning ....
6.3 Declared ratings. conditions and
limitations ..........................
6.4 Tests ..............................
6.5 Compliance with engine and rotor
and power transmission systems
limitations ..........................
6.6 Control of engine rotation .............
6.7 Engine restarting .....................
6.8 Arrangement and functioning ...........
CHAPTER 7 . Instruments and equipment .......
7.1 Required instruments and equipment .....
7.2 Installation ..........................
7.3 Safety and survival equipment ..........
7.4 Navigation lights and anti-collision
lights ..............................
CHAPTER 8 . Electrical systems ..............
CHAPTER 9 . Operating limitations and
information .................................
9.1 General ............................
9.2 Operating limitations .................
9.3 Operating information and procedures ...
Page
IVA-1-1
IVA-1-1
IVA- 1 -2
IVA-2- I
IVA-2- I
IVA-2-1
IVA-2-2
IVA-3-1
IVA-3-1
NA-3-1
IVA-3-1
IVA-3-1
IVA-3-1
IVA-3-2
IVA-3-2
NA-3-2
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IVA-4-1
NA-5-1
IVA-5-1
IVA-5-1
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IVA-6-1
IVAd-1
IVA-6-1
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IVA-6-1
IVA-6-2
IVA-7-1
IVA-7-1
IVA-7-1
IVA-7-1
IVA-7-1
IVA-8-1
IVA-9-1
IVA-9-1
IVA-9-1
IVA-9- 1
9.4 Performance information ..............
9.5 Helicopter flight manual ..............
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附件8--航空器適航性 Airworthiness of Aircraft(4)