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4.2 Responsibilities of Contracting States
in respect of continuing airworthiness .... CHAPTER 8 . Instruments and equipment ......
8.1 Required instruments and equipment ....
8.2 Installation .........................
8.3 Safety and survival equipment .........
8.4 Navigation lights and anti-collision
lights .............................
PART I11 . LARGE AEROPLANES ............
PART IIIA . Aeroplanes over 5 700 kg for which
application for certification was submitted on or
after 13 June 1960. but before 2 March 2004 ..... CHAPTER 9 . Operating limitations and
information ................................
9.1 General ............................
9.2 Operating limitations .................
9.3 Operating information and procedures ...
9.4 Performance information ..............
9.5 Aeroplane flight manual ..............
9.6 Markings and placards ...............
CHAPTER 1 . General .......................
1.1 Applicability ........................
1.2 Number of power.units ................
1.3 Operating limitations .................
1.4 Unsafe features and characteristics ......
1.5 Proof of compliance ..................
IIIA-1-1
IIIA- 1 . 1
IIIA-1-1
IIIA-1-1
IIIA-1-2
IIIA-1-2
ANNEX 8 (iii) 13/12/07
Annex 8 -Airworthiness of Aircruji Table of Contents
CHAPTER 10 . Continuing airworthiness .
maintenance information ...................... IIIA-10-1
10.1 General ............................I IIA-10-1
10.2 Maintenance information .............. IIIA-10-1
10.3 Maintenance programme information .... IIIA-10-1
10.4 Maintenance information resulting
from the type design approval .......... IIIA-10-1
Page Page
CHAPTER 11 . Security ..................... IIIA-11-1
1 1.1 Aeroplanes used for domestic
commercial operations ................ IIIA- 1 1 . 1
11.2 Least-risk bomb location .............. IIIA-11-1
11.3 Protection of the flight crew
compartment ........................ IIIA-11-1
11.4 Interior design .......................I IIA-11-1
PART IIIB . Aeroplanes over 5 700 kg for which
application for certification was submitted on or
after 2 March 2004 .......................... IIIB-A-1
SUB-PART A . General ....... : .............. IIIB-A-1
A.l Applicability ........................ IIIB-A-1
A.2 Opemting limitations ................. IIIB-A-1
A.3 Unsafe features and characteristics ...... IIIB-A-I
A.4 Proof of compliance .................. IIIB-A-1
SUB-PART B . Flight ....................... IIIB-B-1
B.l General ............................ IIIB-B-1
B.2 Performance design parameters ......... IIIB-B- I
B.3 Flying qualities ...................... IIIB-B-2
B.4 Stability and control .................. IIIB-B-3
SUB-PART C . Structure ..................... IIIB-C-1
C.l General ............................ IIIB-C-I
C.2 Mass and mass distribution ............ IIIB-C-1
C.3 Limit loads ......................... IIIB-C-1
C.4 Deformation and ultimate strength ...... IIIB-C-1
C.5 Airspeeds ........................... IIIB-C-1
C.6 Strength ............................ IIIB-C-1
C.7 Survivability ........................ IIIB-C-2
C.8 Structural durability .................. IIIB-C-2
SUB-PART D . Design and construction ........ IIIB-D-1
D.1 General ............................ IIIB-D-I
D.2 Systems design features ............... IIIB-D-1
D.3 Aeroelasticity ....................... IIIB-D-2
D.4 Occupants accommodation features ...... IIIB-D-3
D.5 Electrical bonding and protection against
lightning and static electricity .......... IIIB-D-3
D.6 Emergency landing provisions .......... IIIB-D-3
D.7 Ground handling ..................... IIIB-D-3
SUB-PART E . Powerplant ................... IIIB-E-1
E.1 Engines ............................ IIIB-E-1
E.2 Propellers .......................... IIIB-E- 1
E.3 Powerplant installation ................ IIIB-E-1
SUB-PART F . Systems and equipment .........
F.l General ............................
F.2 Installation .........................
F.3 Safety and survival equipment .........
F.4 Navigation lights and anti-collision
lights .............................
F.5 Electromagnetic interference protection . .
E6 Ice protection .......................
SUB-PART G Operating limitations and
information ................................
G1 General ............................
G2 Operating limitations .................
G3 Operating information and procedures ...
G4 Performance infomation ..............
G5 Flight manual .......................
G6 Markings and placards ...............
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附件8--航空器适航性 Airworthiness of Aircraft(3)
